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Stiffness and vibration properties of slender tensegrity structures

by

Seif Dalil Safaei

September 2012 Technical Reports from Royal Institute of Technology

Department of Mechanics

SE - 100 44 Stockholm, Sweden

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Typsatt i AMS-L

A

TEX

Akademisk avhandling som med tillstånd av Kungliga Tekniska högskolan i Stock- holm framlägges till offentlig granskning för avläggande av teknologie doktorsexa- men torsdagen den 20 september 2012 kl 10.15 i F3, Kungliga Tekniska högskolan, Lindstedsvägen 26, Stockholm.

Seif Dalil Safaei 2012 c

Universitetsservice US–AB, Stockholm 2012

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Stiffness and vibration properties of slender tensegrity structures

Seif Dalil Safaei

Dept. of Mechanics, Royal Institute of Technology SE-100 44 Stockholm, Sweden

Abstract The stiffness and frequency properties of tensegrity structures are func- tions of the pre-stress, topology, configuration, and axial stiffness of the elements. The tensegrity structures considered are tensegrity booms, tensegrity grids, and tensegrity power lines.

A study has been carried out on the pre-stress design. It includes (i) finding the most flexible directions for different pre-stress levels, (ii) finding the pre-stress pattern which maximizes the first natural frequency.

To find the optimum cross-section areas of the elements for triangular prism and Snelson tensegrity booms, an optimization approach is utilized. A constant mass crite- rion is considered and the genetic algorithm (GA) is used as the optimization method.

The stiffness of the triangular prism and Snelson tensegrity booms are modified by introducing actuators. An optimization approach by means of a GA is employed to find the placement of the actuators and their minimum length variations. The results show that the bending stiffness improves significantly, but still an active tensegrity boom is less stiff than a passive truss boom. The GA shows high accuracy in searching the non-structural space.

The tensegrity concept is employed to design a novel transmission power line.

A tensegrity prism module is selected as the building block. A complete parametric study is performed to investigate the influence of several parameters such as number of modules and their dimensions on the stiffness and frequency of the structure. A general approach is suggested to design the structure considering wind and ice loads.

The designed structure has more than 50 times reduction of the electromagnetic field and acceptable deflections under several loading combinations.

A study on the first natural frequencies of Snelson, prisms, Micheletti, Marcus and X-frame based tensegrity booms has been carried out. The result shows that the differences in the first natural frequencies of the truss and tensegrity booms are sig- nificant and not due to the number of mechanisms or pre-stress levels. The tensegrity booms of the type Snelson with 2 bars and prism with 3 bars have higher frequencies among tensegrity booms.

Keywords: Tensegrity booms; Tensegrity grids; Tensegrity power lines; Finite ele- ment analysis; Genetic algorithm; Flexibility analysis; Form-finding; Pre-stress de- sign; Optimization.

iii

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Preface

This work investigates the methods for measuring and improving stiffness of the tensegrity structures. In the first part, a brief introduction and the main underlying research related to tensegrity structures is given. The second part of this thesis is a collection of the following six articles.

Paper 1. D

ALIL

S

AFAEI

, S., E

RIKSSON

, A.

AND

T

IBERT

, G., 2010

“Flexibility-based pre-stress design of tensegrity structures”, Internal report.

Paper 2. D

ALIL

S

AFAEI

, S., E

RIKSSON

, A.

AND

T

IBERT

, G., 2011

“Application of flexibility analysis for design of tensegrity structures”, Proceeding of 4th Structural Engineering World Congress, Como, Italy, 4 −6 April 2011.

Paper 3. D

ALIL

S

AFAEI

, S., E

RIKSSON

, A.

AND

T

IBERT

, G., 2012

“Improving bending stiffness of tensegrity booms”, International Journal of Space Structures, 2012, vol 27 (2-3), 117-130.

Paper 4. D

ALIL

S

AFAEI

, S.

AND

T

IBERT

, G., 2012

“Design and analysis of tensegrity power lines”, International Journal of Space Struc- tures, 2012, vol 27 (2-3), 139-154.

Paper 5. D

ALIL

S

AFAEI

, S., E

RIKSSON

, A.

AND

T

IBERT

, G., 2012

“Optimum pre-stress design for frequency requirement of tensegrity structures ”, Pro- ceeding of 10th World Congress on Computational Mechanics, São Paulo, Brazil, 8 −13 July 2012.

Paper 6. D

ALIL

S

AFAEI

, S., E

RIKSSON

, A., M

ICHELETTI

, A.

AND

T

IBERT

, G., 2012

“Parametric study of various tensegrity modules as building blocks of slender booms”, Submitted to International Journal of Space Structures.

iv

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Division of work between authors

The research project was originally initiated by Dr. Gunnar Tibert (GT) who also acted as the main supervisor and Prof. Anders Eriksson (AE) who acted as advisor. There is a collaboration with Dr. Andrea Micheletti (AM) for paper 6. Seif Dalil Safaei (SD) has continuously discussed the progress of the project throughout the course of the work with AE and GT.

Paper 1

The modeling and simulations were performed by SD with feedback from AE and GT.

The paper was written by SD with input from AE and GT.

Paper 2

The modeling and simulations were performed by SD with feedback from AE and GT.

The paper was written by SD with input from AE and GT.

Paper 3

The modeling and simulations were performed by SD with feedback from AE and GT.

The paper was written by SD with input from AE and GT.

Paper 4

The modeling and simulations were performed by SD with feedback from AE and GT.

The paper was written by SD with input from AE and GT.

Paper 5

The modeling and simulations were performed by SD with feedback from AE and GT.

The paper was written by SD with input from AE and GT.

Paper 6

The modeling and simulations were performed by SD with input from AM and feed- back from AE, GT and AM. The paper was written by SD with input from AE, GT and AM.

v

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vi

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Abstract iii

Preface iv

Part I. Overview and summary

Chapter 1. Aims and scope 1

Chapter 2. Introduction 3

2.1. Statics and kinematics of pin-jointed structures 3

2.2. Definitions of tensegrity 4

2.2.1. Definition 1 4

2.2.2. Definition 2 5

2.2.3. Definition 3 5

2.2.4. Definition 4 5

2.3. Motivating applications 5

2.3.1. Sculpture 5

2.3.2. Domes and roofs 5

2.3.3. Robotics 6

2.3.4. Furniture 7

2.3.5. Space applications 7

2.3.6. Aquaculture 8

2.3.7. Biology 8

2.4. The evolution of tensegrity research 9

2.4.1. Force-finding 10

2.4.2. Form-finding and design 10

2.4.3. Pre-stress effects 10

2.4.4. Stability analysis 13

2.4.5. Vibration analysis 13

2.4.6. Control 13

Chapter 3. Methods 15

Chapter 4. Review of papers 17

4.1. Paper 1 17

4.2. Paper 2 17

4.3. Paper 3 17

4.4. Paper 4 18

4.5. Paper 5 18

4.6. Paper 6 18

vii

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Chapter 5. Conclusions and future works 19

5.1. Conclusions 19

5.2. Future works 20

Acknowledgements 22

Bibliography 23

Part II. Papers

Paper 1. Flexibility-based pre-stress design of tensegrity structures 31 Paper 2. Application of flexibility analysis for design of

tensegrity structures 49

Paper 3. Improving bending stiffness of tensegrity booms 59 Paper 4. Design and analysis of tensegrity power lines 83 Paper 5. Optimum pre-stress deisgn for frequency requirement of

tensegrity structures 111

Paper 6. Parametric study of various tensegrity modules as

building blocks for slender booms 125

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Part I

Overview and summary

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CHAPTER 1

Aims and scope

Tensegrity structures have been the subject of research for many years. For terrestrial applications the following steps must be mastered to convey an idea to reality for any application:

• Form-finding: tools to find the equilibrium configurations of a wide variety of topologies and configurations are available, and the form-finding step can no longer be considered as a major problem of tensegrity structures. As numerous robust methods are available.

• Pre-stress design and stability evaluation: the methods to compute the states of self-stress, and investigate the behavior of the tensegrity structures from equilibrium and stiffness matrices are available.

• Static and dynamic analysis: although the analysis of the tensegrity structures as a non-linear system is complex, the methods are available to compute the non-linear response of the structure.

• Manufacturing: manufacturing of tensegrity structures has generally been given very little attention. The reason might be due to the low structural efficiency of tensegrity structures or to manufacturing problems, e.g., pre-stressing.

As methods for analyzing tensegrity structures already are available, the aims of the present work is to investigate the possibilities and potential of tensegrities for ter- restrial and space applications. A number of research has been done on double-layer tensegrity grids and domes, resulting in a deeper understanding about their behav- ior, but less work has been done on tensegrity masts, towers and booms, despite the fact that several tensegrity towers have been built. This work thus mainly focuses on slender beam-like tensegrity structures to investigate their bending stiffness and, if required, ways to improve their stiffness to evaluate their usefulness for different terrestrial and space applications requiring slender beam-like structures. Hence, the study has a strong focus on applicability of tensegrity structures and combines rele- vant state-of-the-art analysis methods to achieve the aims. Another driving factor has been to simplify and visualize the presentation of the results of the analyzes so that conclusions can be drawn and to provide a better understanding of the fundamental behavior of slender tensegrity structures.

In order to achieve the above aims, the following work was performed:

• A finite element program was developed for non-linear static and linear dy- namic analysis of general tensegrity structures.

1

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2 1. AIMS AND SCOPE

• The flexibility analysis was introduced and employed as a tool for visual com- parison of the flexibility of general tensegrity structures.

• The influence of the pre-stress level on the most flexible directions, first nat- ural frequency and mode shapes of various tensegrity modules and slender tensegrity structures were studied.

• The influence of infinitesimal mechanisms on the first natural frequency of several slender booms was investigated.

• Optimization was performed for pre-stress selection to maximize the first nat- ural frequency of different tensegrities.

• Actuators were used for stiffness modification of tensegrity booms when cable slackening occurred.

• Optimization was used to find the stiffness of the Snelson and prism type tensegrity booms for a constant mass criterion.

• The influence of the number of modules along the length on the stiffness was investigated.

• The tensegrity concept was used to design new transmission power lines with lower electromagnetic field than current designs.

• The influence of wind and snow loads on the stiffness and frequency properties of the slender tensegrity power lines were studied.

• A risk analysis on the effects of a single element loss of the tensegrity power lines was performed.

• A study was performed on the applicability of slender tensegrity booms for

space applications.

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CHAPTER 2

Introduction

Tensegrity is an artificial word, composed of the two expressions tensional and in- tegrity. There is a controversy about the origin of tensegrity structures, but the archi- tect Richard Buckminster Fuller and artist Kenneth Snelson are known as the inventors of the tensegrity idea (Wroldsen 2007; Snelson 2012). The tensegrity is a structural concept with many different applications.

2.1. Statics and kinematics of pin-jointed structures

Understanding the concepts of statical and kinematical determinacy are central to an understanding of the mechanics of pin-jointed frameworks like tensegrity structures.

The static equilibrium for a three-dimensional pin-jointed framework with j joints, b members, and c kinematic constraints is:

At = f (2.1)

where A is the equilibrium matrix, t the internal forces of the members and f the vector of the external load. The equation of kinematics of small displacement is:

A

T

d = e (2.2)

where A

T

is the kinematic matrix and e is the elongation. Once the rank r of the equilibrium matrix has been found, the number of states of self-stress and mechanism are (Pellegrino 1993):

s = b − r (2.3)

m = 3j − c − r (2.4)

Tensegrity structures belong to the class of statically indeterminate structures. One can think of indeterminacy in terms of states of self-stress that is a set of member forces in static equilibrium with zero external load. Structures composed of tension elements (strings, tendons or cables) and compression elements (bars or struts) in equilibrium are often denoted as tensegrity structures (Fig. 2.1).

The design process of tensegrity structures includes the simultaneous finding of a suitable geometry, topology, element axial stiffness, and the initial self-stressed state.

3

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4 2. INTRODUCTION

In a study of the force displacement relationship (static and dynamic analysis), it is essential to understand how the structure behaves when subjected to external loads, but also to find the new stable configuration under such conditions.

m=0 s=1

1 2

4 3

Figure 2.1: X-frame tensegrity structure with one state of self-stress and no mecha- nism

2.2. Definitions of tensegrity

Several definitions of tensegrity structure have been formulated, reflecting different purposes. Below, some of the more recent ones are discussed.

2.2.1. Definition 1 Motro and Raducanu (2003) define tensegrity structures as:

Tensegrity systems are spatial reticulate systems in a state of self-stress. All their elements have a straight middle fiber and are of equivalent size. Tensional elements have no rigidity in compression and constitute a continuous set. Compressed elements constitute a discontinuous set. Each node receives one and only one compressed ele- ment.

The term ”spatial reticulate systems in a state of self-stress” tells us that tensegri-

ties are composed of tension and compression elements. This definition is very strict,

and there seems to be little reason for limiting the definition to elements with equiv-

alent sizes. There is no need to have ”one and only one compressive member in each

node”. For example, the tensegrity boom of type T-3 has two compressive elements in

each node.

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2.3. MOTIVATING APPLICATIONS 5 2.2.2. Definition 2

Hanaor (1994) defines tensegrity structures as:

Internally pre-stressed, free standing pin-jointed networks in which the cables are tensioned against a system of bars.

This is a wider definition, but it is difficult to distinguish tensegrity from other pre-stressed reticulate systems.

2.2.3. Definition 3

Skelton et al. (2001) define a class K tensegrity structure as:

A stable structure composed of tension and compression elements with a maxi- mum of K compressive members connected at the node(s).

This definition expands the definitions of tensegrity to include structures which have more than one compressive element at each node.

2.2.4. Definition 4 Fuller (1975) defines tensegrity structure as:

Islands of compression in a sea of tension.

This definition says that a few compressive elements are located among a larger number of tension elements (Fig 2.2). Tensegrity describes a structural principle in which the structural shape is guaranteed by comprehensively continuous, tensional behavior of the system and not by the discontinuous and exclusively local compres- sional member behavior.

2.3. Motivating applications

In this section, some applications of the tensegrity concept will be briefly reviewed.

2.3.1. Sculpture

The artist Kenneth Snelson has since he invented tensegrity structures developed an amazing collection of artwork (Fig. 2.2) exhibited in different parks and museums (Snelson 2011).

2.3.2. Domes and roofs

The tensegrity concept has also found more traditional applications within architec-

ture and civil engineering, such as large dome structures, stadium roofs, temporary

structures and tents. The well known Munich Olympic Stadium designed by Frei Otto

for the 1972 Summer Olympics, and the Millennium Dome by Richard Rogers for

celebrating the beginning of the third millennium are both tensile structures, close to

the tensegrity concept with so-called flying masts. The Seoul Olympic Gymnastics

Hall, for the 1988 Summer Olympics, and the Georgia Dome, for the 1996 Summer

Olympics, are examples of tensegrity concepts in large structures (Wroldsen 2007).

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6 2. INTRODUCTION

Figure 2.2: Snelson artworks of tensegrity structures. Courtesy of Kenneth Snelson (www.kennethsnelson.net)

Figure 2.3: Georgia Dome. Reproduced from www.gadome.com.

2.3.3. Robotics

Recently, there has been a high interest in biologically inspired robotic systems, e.g.

snake robots. Tensegrity robots are an excellent example of such systems, as they

utilize a number of actuators and degrees of freedom. Tensegrity robots can be light-

weight, when using strings as tensile components, and therefore also fast, due to low

inertia. Using a large number of controllable strings potentially makes them capable

of delicate object handling. Also, it is believed that low control energy is needed to

change the configuration of tensegrity structures. Thus, a shape change can be done

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2.3. MOTIVATING APPLICATIONS 7 with much lower cost than for traditional structures, cf., Shai et al. (2010), Rieffel et al. (2010), Tur (2010), Schmalz and Agrawal (2009), Juan et al. (2009), Shibata et al. (2009), Juan and Mirats Tur (2008a), Ladjal et al. (2008), Yu et al. (2008), Voisembert et al. (2011), Moored et al. (2011).

2.3.4. Furniture

The principle of tensegrity proposes many possibilities in the design of furnitures (Fig.

2.4), as it leads to lightweight new designs.

Figure 2.4: Tensegrity furnitures. Reproduced from www.intensiondesigns.com

2.3.5. Space applications

Tensegrity structures, as compactly packable deployable structures, are interesting for space applications. The most common structures using this concept are masts, anten- nas, and solar arrays (Tibert 2002). Most research in this area focuses on deployment.

Tibert (2002) provides a thorough review of existing technologies. They are suitable candidate for space application as (Juan and Mirats Tur 2008b):

• They do not contain hinges or rotational joints, which are the sources of un- wanted friction.

• With a minimal number of bars, they have the potential to be packaged to very small volumes.

• Tensegrity structures are attractive from control point of view.

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8 2. INTRODUCTION

Figure 2.5: ADAM deployment sequence (Courtesy of AEC-Able Engineering Com- pany, Inc.).

ABLE Engineering (www.ableengineering.com ) is one manufacturer of the above concepts, denoting them continuous longeron booms and the articulated longeron booms. There are two possible deployment schemes, one using the internal energy of the stowed structure, and another one using additional motors.

2.3.6. Aquaculture

An extensive use of the tensegrity concepts in future aquaculture installations could improve system solutions (Wroldsen 2007). The inherent flexibility of tensegrity structures could be taken advantage of to design wave compliant installations. By distributing the environmental loading throughout the entire structure, one could re- duce the traditional problems of having load concentrations in a few connectors. The slender elements could contribute to reduce the drag compared with existing designs.

However, the greater portion of the environmental loading is introduced through nets, and not the supporting frame. The rod elements could be realized as hollow pipes pro- viding sufficient buoyancy through a large number of distributed and relatively small floaters.

2.3.7. Biology

Tensegrity structures can be seen as inspired by biological load carrying structures.

Ingber (2008a,b) presents the geodesic forms in groups of carbon atoms, viruses, en- zymes, organelles, cells and even small organisms, and emphasizes the point that these structures arrange themselves, to minimize energy and mass, through applying the principle of tensegrity.

The tensegrity principle is also found in the strongest fiber in nature (Termonia

1994), which is the silk of spider, where hard pleated sheets take compression and a

network of amorphous strains take tension.

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2.4. THE EVOLUTION OF TENSEGRITY RESEARCH 9 The human body, and in particular the musculo-skeletal system, is itself built on the principle of tensegrity. At a macroscopic level we have 206 bones, in compression, stabilized by approximately 639 muscles, in tension. Tensegrity structures are thereby also very similar to muscle-skeleton structures of highly efficient animals or humans (Wroldsen 2007).

The tensegrity principle has been used to explain numerous phenomena within the behavior of cells and molecules. One example is the linear stiffening of isolated molecules, such as the deoxyribonucleic acid (DNA). The stiffness of tissues, living cells and molecules is altered by changing the internal level of self stress (Ingber 2008a,b). The understanding of how cells sense mechanical stimuli and how they regulate the growth of tissue could be used to accelerate molecular modeling and drug design.

Common patterns, such as triangulated forms, are used to build a large diversity of structures. Snowflakes, soap bubbles, bee honeycombs, the wing of a dragonfly, leafs of trees, cracked mud, the skin of reptiles and a bumblebee’s eye are some examples of tensegrity structures in biology (Pearce 1990).

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Figure 2.6: (a) Pelvis Schematic, (b) Tensegrity Octet Pelvis, (c) Foot Construction, (d) Tensegrity Knee Construction. Reproduced from www.biotensegrity.com.

2.4. The evolution of tensegrity research

Mirats Tur and Juan (2009) classify the main underlying problems of tensegrity struc-

tures as form-finding, static analysis, dynamic analysis, shape control and control of

vibration. Here, we provide a more accurate classification, since design, static and

dynamic analysis cover a broad subject within tensegrity structures, and some times

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10 2. INTRODUCTION

they overlap. For example, form-finding is mostly seen as a step in the design process of tensegrity structures, but it can also be a part of static analysis.

2.4.1. Force-finding

The process of finding initial member forces for a given geometry is known as pre- stress design. Pellegrino (1993) shows how the basis for the pre-stress state is ob- tained from the null space of the equilibrium matrix. Quirant (2007) expands the method by Pellegrino and Calladine (1986) to tensegrity structures by considering the unilateral behavior of the cable elements, and also presents a method for choosing ac- tive elements for tension setting. The method is different from the method by Kwan and Pellegrino (1993), which tries to minimize the total member elongation for op- timal placement of actuators. Based on the method by Quirant (2007) and Quirant et al. (2003) for finding the feasible self-stress mode, Tran and Lee (2010b) present a method for finding a single self-stress mode taking into account the unilateral proper- ties and the stability of the structure. Xu and Luo (2010a) use a simulated annealing algorithm to solve an optimization model for the pre-stress design. Even though a number of studies have been performed for initial pre-stress design, no systematic study has given methods for finding the least magnitude of pre-stress depending on magnitude, direction and position of external loads, and functional criteria such as limited displacement and sufficient overall stiffness.

2.4.2. Form-finding and design

The process of determining a topology and a geometric shape is known as form- finding. Tibert and Pellegrino (2003) review form-finding methods. Table 1.1 gives a summary of different form-finding methods initiated by Juan and Mirats Tur (2008b) and extended by present author. Most of the proposed methods for form-finding do not consider self-weight and external forces. Hanaor (2011) review the main features of the design of double layer grids emphasizing unusual behaviors which require special attention in design.

2.4.3. Pre-stress effects

Pre-stress effects in tensegrity structures are mostly seen as part of a static analysis, but this section also reviews their influence on the dynamic behavior of tensegrity structures.

An important characteristic of tensegrity structures is their geometric stiffening, i.e., that the stiffness increases when external forces are applied, or equivalently, when infinitesimal mechanisms are activated.

Levy et al. (1994) perform an experimental study of pre-stressing in double layer grids, and shows that the efficiency of the structure increases by pre-stressing the structure.

Perhaps one of the most important studies regarding pre-stress is done by Skelton et al. (2001). They study various tensegrity structures and show some general proper- ties of tensegrity structures. Their important results are the following (Skelton et al.

2001):

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2.4. THE EVOLUTION OF TENSEGRITY RESEARCH 11

T able 2.1: Summary of form-finding methods Method name References Class Stability Initial config- uration Symmetry Initial topology External forces Analytic solution (Connelly and T errell 1995) Kinematic No No Y es Y es No Non-linear program- ming (Pelle grino and Calla- dine 1986) Kinematic No Y es No Y es No Dynamic relaxation (Motro 1984) Kinematic Y es Y es No Y es Y es Analytic solution (K enner 1976) Static Y es Y es Y es Y es No F orce-density method (Linkwitz 1999) Static Must be gi v en No No Y es Y es Ener gy method (Connely 1993) Static Y es No No Y es No Reduced coordinates (Sultan et al. 1999) Static Y es No Y es Y es No Dif ferential equations (Micheletti and W illiams 2004) Static Y es Y es No Y es No Successi v e approxi- mation (Zhang et al. 2006) Both Some stresses ha v e to be fix ed Some coordi- nates ha v e to be fix ed

No Y es No Algebraic method (Masic et al. 2005) Static Must be gi v en No No Y es Y es Genetic algorithm (P aul et al. 2005) T opologic Y es No No No No Sequential quadratic programming (Masic et al. 2006) Both Y es No No No Y es Numerical method (Estrada et al. 2006) Both Y es No No Y es No FEM method (P agitz and Mirats T ur 2009) Static Y es Y es Y es YES Y es

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12 2. INTRODUCTION

• ”When no string is slack, the geometry of a tensegrity and the material used have much more important effect on its stiffness than the amount of pre-tension in its strings.”

• ”Pre-tension can be used to maintain a constant bending rigidity over a wider range of external loads. This can be important when the range of external loads can be uncertain.”

Murakami (2001) studies static and dynamic characterization of the spherical tensegrity module invented by Buckminster Fuller. He defines nodal coordinates and connectivity by using graphs of an icosahedral group. The pre-stress mode shows that cable tension is always less than the absolute value of bar compression. He also demonstrates that natural frequencies of infinitesimal mechanism modes increase pro- portionally to the square root of amplitude pre-stress.

Sultan et al. (2001) study pre-stressability conditions of tensegrity structures un- der the following assumptions:

• All the joints of the system are affected by kinetic friction.

• Tendons are affected by kinetic damping.

• All constraints are scleronomic and bilateral. In other words, they are not time dependent and they are not mathematically expressed as inequalities.

• The constraint forces do no mechanical work.

Under these conditions they define the general prestressability conditions. A necessary and sufficient condition for the static equilibrium is that zero virtual work is done by the applied forces in moving through an arbitrary, reversible, virtual displacement satisfying the constraints.

Defossez (2004) studies the mechanical response of a symmetric tensegrity struc- ture to an external constraint when the structure is close to its tensegrity limit above which its collapses. A numerical analysis is employed to minimize the internal elastic potential energy function. Although the hypothesis of the model restricts this study to the theoretical case, two non-linear effects are found:

• The mechanical power response of the tensegrity structure can be modulated according to the magnitude of the applied force. This indicates that the struc- ture may act as a mechanical power amplifier.

• A slightly pre-stressed tensegrity structure can offer a greater load carrying capacity to an applied force than pre-stressed equivalent structures. This para- doxical stiffening indicated that increasing the pre-stress may not always be the most efficient way to keep the stability of the structure.

A very interesting result, presented by Sultan et al. (2002), is that the difference

between the complete non-linear dynamic model and its linearized version at an equi-

librium configuration decreases as the pre-stress of the cables increases, demonstrated

for Snelson tensegrity structures. For two classes of tensegrity structures, linear equa-

tions of motion around a reference solutions are derived by Sultan et al. (2002). The

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2.4. THE EVOLUTION OF TENSEGRITY RESEARCH 13 results from numerical experiments show that linear kinetic friction is enough to as- sure asymptotical stability of configurations.

2.4.4. Stability analysis

Connelly (1999) introduces a stability criterion called super stability. Lazopoulos (2005) studies the stability of a T-3 tensegrity structure for both global instability and buckling, and derives the mathematical formulation of instability. Ohsaki and Zhang (2006) study stability conditions of tensegrity structures. For a two-dimensional tenseg- rity structure, positive definiteness of the reduced form of the geometrical matrix is a necessary but not a sufficient condition for the stability of the structure. A sufficient condition for tensegrity can be rigorously defined by the eigenvalues and eigenvectors of linear and geometrical matrices. Jensen et al. (2007) study several combinations of pre-stress and axial stiffness of a tensegrity beam to show the influences on the resulting stiffness.

2.4.5. Vibration analysis

Regarding the oscillatory behavior of tensegrity structures, several researchers, such as Furuya et al. (2006) and Oppenheim and Williams (2001) for a simple highly sym- metric tensegrity, Moussa et al. (2001) for a kind of modular tensegrities, or Sultan et al. (2002) for SVD tensegrity structures, have shown that the frequencies of the oscillation modes of a tensegrity structure increase with the pre-stress levels. Mu- rakami (2001) also studies this for simple prismatic tensegrities, and concludes that the increase is proportional to the square root of the pre-stress. This result opens the possibility to adjust the resonance frequency of the structure to meet specific re- quirements. Another important result regarding the oscillation modes of a tensegrity structure, shown by Motro et al. (1986), is that the geometric flexibility of the structure leads to a slower decay of vibrations than the expected exponential decay. Some au- thors have simulated the behavior of the tensegrity structure under perturbations, not requiring an explicit solution of the dynamic model. Analytical methods for the simu- lation of such structures are classified by Barnes (1999) into incremental, iterative and minimization methods. Incremental and iterative methods use the matrix formulation of finite elements. For instance, Furuya et al. (2006) divide the structure into a large set of small, simpler, linked elements, and then apply the problem constraints to all of them. On the minimization side, a widely used method is the dynamic relaxation method. Domer et al. (2003) study the tensegrity geometric non-linearities by using neural networks to improve the accuracy of the dynamic relaxation method. Oppen- heim and Williams (2001) show that natural geometric flexibility leads to inefficient mobilization of the natural damping in the elastic cables. This effect results in a much slower rate of decay of amplitude of vibration than might be expected.

2.4.6. Control

Because of inaccuracy in the dynamic model, and also unknown perturbations, the

structure most likely will have some oscillation around the equilibrium. In order to

minimize or reduce this undesired effect, some kind of control must be used. This

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14 2. INTRODUCTION

review is related to active control when actuators and sensors are utilized through feedback control.

Djouadi et al. (1998) propose a method for active control of tensegrity systems.

A closed-loop instantaneous optimal control algorithm was proposed and applied to structures undergoing large displacements. Also, trajectories of special nodes, maxi- mum displacements of nodes, maximum and minimum stresses in cables, and maxi- mum control forces of the actuator were studied.

Chan et al. (2004) built a three-stage tensegrity tower with piezoelectric force sensors and displacement actuators. This structure was mounted on a shaker table which provides vibration to the bottom of the structure. The objective was to reduce the vibration of the top nodes. Acceleration and local internal force feedback control were used for control of vibration. It is shown that both controllers perform well and are able two damp the first to bending mode by 20 dB, but acceleration feedback control has better performance.

For a two stage, three-strut tensegrity structure, Raja and Narayanan (2007) pro- pose a method with full state and partial force feedback control for stationary and non-stationary excitation. The dynamic analysis of the tensegrity structure including the piezoelectric actuators was carried out using finite element analysis. It is found that H

controller is more effective than H

2

controller in terms of displacement.

A search for the best among all possible actions is utilized in methods based on artificial intelligence. Thus, given the desired and current configuration of the structure, the problem is to find the best combination of actions to reduce the error (Adam and Smith 2007). The input to the system consists of a set of performance goals. The major tasks of the systems are: (a) comparison of the current structural state with desired performance goals; (b) searching for a set of control actions that improve the performance; (c) evaluation of the selected solution; (d) execution of a set of actions; (e) measurement of the behavior of the new structural state, and finally (f) utilization the current event as an instance for learning and planning (Shea et al. 2002).

In this framework, apart from the search for the best action, learning techniques are used to improve the needed computational methods. The first advantage of this method is that there are strong interactions between active features and overall behavioral properties (Adam and Smith 2007) .

Designing first a structure, and then its control is not an efficient way of achieving a good performance, since the design of the structure ignores its controllability, usually yielding structures with severe limitations. In order to avert this problem, Masic et al.

(2005) study the optimal mixed dynamic and control performance through pre-stress

optimization. For pre-stress parameterization, they used force density variables which

appear linearly in the model.

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CHAPTER 3

Methods

Detailed descriptions of all methods used in this thesis are given in the paper section.

A summary of these methods is given.

A finite element (FE) based method is used to solve the non-linear quasi-static equilibrium problem. The method presented by Guest (2006) is utilized for tangent stiffness formulation throughout the thesis. The method utilizes a modified axial stiff- ness for a pre-stressed bar. Stiffness formulations of the tension and compression elements are equal as long as tension elements are in tension, but the stiffness of the tension elements is considered to be zero when they are slack. The material and geo- metric stiffness together can be used to give the correct structural tangent stiffness matrix. The stiffness formulation is certainly not new, but a novel feature is the use of a modified axial stiffness, which for conventional structures is little different from the conventional axial stiffness. The result is compared with the stiffness matrix for- mulation presented by Pagitz and Mirats Tur (2009). The Newton-Raphson method is employed to deal with the non-linear quasi-static equilibrium formulation. The FEM program is developed to be as general as possible with nodal coordinates, elements connectivity, and a pre-stress pattern as input. The program is able to handle both plane and spatial structures.

Singular Value Decomposition (SVD) is applied to the equilibrium matrix to find the basis of self-stress state (Pellegrino 1993). The studies by Calladine and Pellegrino (1991) and Pellegrino (1990) are employed for finding the equilibrium matrix, the state of self-stress and the number of mechanisms. We implemented the method presented by Tran and Lee (2010b) for finding a feasible self-stress state. They considered the unilateral properties of stresses in cables and struts, and also evaluated the stability of the tensegrity structures. In this method, elements are classified in different groups based on the symmetry of the structure to obtain a single feasible pre-stress state, but it is noted that alternative pre-stress patterns are possible for all tensegrities with a null space of equilibrium of order higher than one.

The concept of flexibility ellipsoids is introduced by Ströbel (1995). New ap- plications of flexibility ellipsoids were introduced, where the flexibility ellipsoids are utilized to find the most flexible directions of a given structure, but also for compari- son of different structures, and as a way to measure the effect of disturbances on the structure. The concept of flexibility ellipsoids is expanded to consider non-linearity.

In this case, a finite external load is rotated around each free node and all nodal dis- placements are measured and drawn. The non-linear form of flexibility ellipsoids is denoted flexibility figures and are utilized for finding the real most flexible direction of

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16 3. METHODS

the structure considering different pre-stress levels, and consequently the magnitude of external load. We also introduce the incremental flexibility as a means for stability evaluation of loaded structure. In this case, a differential force is similarly rotated around the nodes.

A genetic algorithm (GA) is utilized in different stages of optimization of the structures studied. A genetic algorithm is a search heuristic that mimics the process of natural evolution, and it is an appropriate method for searching non-structural space with many constraints and not a high demand for accuracy. This heuristic is rou- tinely used to generate useful solutions to optimization and search problems. Genetic algorithms belong to the larger class of evolutionary algorithms (EA), which gener- ate solutions to optimization problems using techniques inspired by natural evolution, such as inheritance, mutation, selection, and crossover. We used the GA optimization toolbox of Matlab for the simulation. We set different values for selection, cross over, and mutation. A new technique is here employed to select design variable bounds to prevent singularity of tangent stiffness matrix. The GA is employed to find (i) the op- timum cross-section areas of the boom elements for a constant mass criterion, (ii) to find the optimum placement of actuators and their optimum actuation for improving stiffness of the tensegrity booms, (iii) to find the optimum self-stress states regarding the frequency requirement.

Simple and complex tensegrity units are studied. Three-dimensional tensegrity

structures are composed of various bars held together by cables to form a tensegrity

unit. The tensegrity modules of the types X-frame based, Snelson, prism, Micheletti,

Marcus are studied in this work.

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CHAPTER 4

Review of papers

4.1. Paper 1

The aim of this study was to find a method to establish a suitable pre-stress level for a general tensegrity structure. A tool based on non-linear flexibility analysis is provided to find the most flexible directions of the structures. The nodes which have the largest displacements, are more important for design. The designer is able to find the critical load combinations for pre-stress design. A critical load combination is the one which creates larger displacements. In addition, a loaded structure should have limited displacements regarding disturbances. Therefore, the linearized form of flexibility analysis was used to find the deformation of a loaded structure under incremental loads.

4.2. Paper 2

In this study, the flexibility analysis was extended to consider space structures. We utilized this method to compare T-3 and Snelson tensegrity structures. The important result of this paper is the possibility for finding the most flexible directions of tenseg- rity structures depending on different pre-stress levels, and load magnitude. It was found that the pre-stress has an important role in changing the most flexible direc- tions of the structure. It was shown that the methods based on linear analysis of the equilibrium matrix does not find the most flexible direction.

4.3. Paper 3

The aim of this study was to improve the bending stiffness of tensegrity booms. Flex- ibility ellipsoids show that tensegrity booms have low bending stiffness. The first step was to develop a strategy for a fair comparison of a commercial truss boom with tensegrity booms. Finite element analysis was employed for non-linear static analysis and GA for optimization. An optimization algorithm is formulated to determine the cross-section areas of the compressive and tension elements. Pre-stress is connected to local buckling of compressive elements, since bar buckling happens earlier for typ- ical component properties. Results show that tensegrity booms are less stiff than a truss boom, as expected. In addition, the effect of the safety factor against bar buck- ling on the stiffness is studied. To improve the stiffness, the possibility of employing actuators is searched. Two different strategies were employed to find the placement of actuators for tensegrity booms. An optimization algorithm was then formulated to

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18 4. REVIEW OF PAPERS

find the minimum required length variation of each actuator. Results are promising, indicating a significant improvement in the bending displacement.

4.4. Paper 4

The tensegrity concept is employed to design a new type of transmission power lines.

It has been shown that the modules of the type T-n is suitable due to their simplicity and providing the configuration twist crucial for reduction of the electromagnetic field.

The form-finding routine is able to create various structural shapes. An extensive parametric study has been performed to investigate static and dynamic behavior of the proposed structure. The designed structure, 100 m long, has high stiffness against various loading conditions such as self-weight, ice loads and wind loads with and more than 50 times electromagnetic field reduction.

4.5. Paper 5

A tensegrity structure as a statically indeterminate structure may have several states of self-stresses. The singular value decomposition of the equilibrium matrix provides the bases of self-stress. This study was an effort to connect the bases of self-stress to pre-stress level and frequency of the structure. A genetic algorithm is used to find the optimum self-stress pattern for each pre-stress level to maximize the first natural frequency of the structure.

4.6. Paper 6

There is a high demand for long, slender and ultra-lightweight deployable booms for

space missions. Although it is known that the tensegrity booms have lower first natural

frequency than truss booms, it is important to quantify how much lower frequencies

they have. The first natural frequency is selected for comparison, since it contains

both the stiffness and mass properties of the booms. This paper shows that the first

natural frequency of the tensegrity booms are significantly lower than that of the truss

booms. It is also shown that a pre-stress level increment cannot significantly enhance

the frequency properties of the tensegrity booms. The low frequencies of the tensegrity

booms are thus not due to the infinitesimal mechanism as a structure with a larger

number of mechanisms may have higher first natural frequency.

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CHAPTER 5

Conclusions and future works

5.1. Conclusions

Non-linear flexibility analysis is found to be a proper method for finding the most flexible directions of tensegrity structures and their dependence on different pre-stress levels. It was shown that the most flexible directions are dependent on pre-stress levels and that the methods based on linear analysis such as SVD analysis of the equilibrium matrix or flexibility ellipsoids are no longer valid for highly pre-stressed structures.

Flexibility figures are useful tools for determining the critical load combinations and for finding the cable with the highest probability of going slack under external load. In addition, they are useful tools for a complete stiffness comparison of different struc- tures.

A strategy was developed to give a fair comparison between tensegrity booms and a commercial truss boom. The results show that the tensegrity booms have lower stiffness in a typical bending application. The buckling safety factor of compres- sive elements has an important role on the stiffness. A large safety factor results in more material in compressive elements, and, consequently, less material for tension elements. Thus, the axial stiffness of the tension elements gets lower resulting in a reduction of the bending stiffness of the structure for a given mass. In other words, increasing the buckling safety factor decreases the stiffness of the structure. The ad- vantage of increasing buckling safety factor is a higher capacity for pre-stressing.

An effort is made to enhance the stiffness of the 10-stage T-3 and Snelson booms when a number of cables are slack. Five and six actuators are considered for the T- 3 and Snelson booms, respectively. Different examples show that small unstrained lengths variations are sufficient to change the configuration of the structure, a unique property of the tensegrity structures.

The tensegrity concept is used for the design of novel transmission power lines which reduce the electromagnetic field. A tensegrity prism with 3 bars is selected as the building block of the structure. An effort is made to investigate the influence of varying number of modules and structural dimensions. Changing the number of mod- ules results in changing the most flexible directions which have significant influence on the stiffness and frequency properties of the structure. The influence of various loading situations such as self-weight, wind and ice loads are studied on the 100 m structure. The designed structure shows a 52 times reduction of the electromagnetic field and low deformation under real loading situations.

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20 5. CONCLUSIONS AND FUTURE WORKS

The interesting result from paper 5 is that the pre-stress patterns differ for various pre-stress levels. A designer should select the pre-stress pattern which results in the highest performance. This approach is different to the traditional one in that the se- lection of pre-stress and post analysis are conducted in two different stages. The GA again shows high performance of finding the optimum pattern.

The new aspect of the research in papers 3 and 5 was a link between FEM and GA, where values of the objective function and constraints are obtained by FEM, and GA is employed as the optimization tool. Genetic algorithm has shown high accuracy of searching the design space, and in finding the minimum actuation.

This work is aimed to extensively investigate the capability of tensegrity concept for space boom applications. Although many studies shows that tensegrity structures are more flexible that conventional trusses, it is interesting to show how much more flexible they are. The investigation was based on a natural frequency comparison of the various tensegrity booms with state-of-the-art truss boom. The results shows that the first natural frequency of the tensegrity booms are orders of magnitude lower than that of the truss booms. The role of infinitesimal mechanisms is investigated, and it is shown that the low frequency properties of the tensegrity booms is not due to the number of mechanisms, but on the geometry. In addition, the influence of pre-stress levels on the first natural properties of the tensegrity booms is studied. The result shows that the higher pre-stress increases the first natural frequency, but its effect is limited.

5.2. Future works

In this section, I would like to discuss about the future of tensegrity structures. A number of studies has been performed and a number of articles have been published on the tensegrity structures, but only very few of them have been built as a load carrying structure. I think now is the time to raise important questions: What is the main aim of tensegrity research? My personal view is that research should be conveyed to find out potential applications. This only happens when one carefully investigates the properties of the tensegrity structures without personal exceptions or wishes.

• At the age of virtual reality where computers make the realization of almost any shape possible, more and more shapes are emerging. We change the pre- stress level easily by typing a different number. How can the complex shapes be manufactured? Is it possible to increase the pre-stress when the structure is built? How to repair the structure, if there is a damage in certain elements?

How sensitive is various shapes to inaccuracies of their geometry? I think there should be more consideration regarding manufacturing aspects of tensegrity structures.

• With respect to terrestrial applications, a tensegrity is exposed to environmen-

tal loads, e.g., wind loads. A few studies have been performed to investigate

the influence of various loading situations. A tensegrity structure sensitive to

imperfections of the geometry may become unstable for a sudden changes in

temperature. In addition, it would be interesting to investigate the taut-slack

transition of the tensegrity structures under vibrations.

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• Due to low stiffness of the tensegrity structures, the performance of the struc- ture degrades. For example, it would oscillate when it is supposed to remain still or it will not follow the desired path. In order to eliminate, or at least minimize these undesired effects, it is necessary to use some kind of control technique. Sensors and actuators can be employed, and using the knowledge about the structure dynamics, feedback control can be designed.

• I think, tensegrities are well fit for robotic and specific space applications where flexibility and shape control is required. It is proven that a small change in unstressed length of one cable can change the shape of the structure. We im- proved the stiffness of the ten-stage Snelson tensegrity boom with introducing 6 actuators on saddle cables of certain stage with very small change in un- stressed length of the cables. In this case, with few actuators, a shape change can be obtained.

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Acknowledgements

The work finally ended in this PhD thesis which was made possible by support from supervisors, colleagues, friends and family. I give my sincere gratitude to:

Dr. Gunnar Tibert my main supervisor, for introducing me to the field of tenseg- rity. Your patience, support, assistance and guidance helped me to overcome the prob- lems I have experienced. I would also like to thank you for being a friend but still being decisive in your leadership.

I would like to thank Prof. Anders Eriksson my co-supervisor. Your guidance and sharing the knowledge had a major role on accomplishing this work. But I would like to emphasize your positive attitude which gives a high confidence to the students.

Throughout this period, I enjoyed the good atmosphere at KTH Mechanics, es- pecially in our research group. Thanks to my room mates Erik, Krishna and Robert.

Special thanks to Andreas Vallgren and Hans Silverhag.

There were a number of people who supported me during this time to accomplish this work. Maryam and Akbar, my aunt and uncle, supported me from the time I remember. Naser and Mansour, my twin uncles, were always ready when I needed help and came with incredible support. I definitely do not forget my cousins, Seif, Yalda and Azin who always shared their nice feeling with me.

I thank Sahar and her spouse, Navid who provided nice moments and great atmo- sphere at home when I was in Sweden. Finally but most importantly, to my parents, Ali and Sima, who have always been my motivation and inspiration, even though they cannot be with me in Sweden.

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