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Adaptive aeroservoelastic control / / Ashish Tewari
Adaptive aeroservoelastic control / / Ashish Tewari
Autore Tewari Ashish
Pubbl/distr/stampa Chichester, England : , : Wiley, , 2016
Descrizione fisica 1 online resource (482 p.)
Disciplina 629.132/6
Collana Aerospace Series
Soggetto topico Airplanes - Control systems
Aeroservoelasticity
Adaptive control systems
ISBN 1-118-92773-7
1-118-92772-9
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Aerospace Series List; Title Page; Copyright; Dedication; Table of Contents; About the Author; Series Editor's Preface; Preface; Chapter 1: Introduction; 1.1 Aeroservoelasticity; 1.2 Unsteady Aerodynamics; 1.3 Linear Feedback Design; 1.4 Parametric Uncertainty and Variation; 1.5 Adaptive Control Design; 1.6 Organization; References; Chapter 2: Linear Control Systems; 2.1 Notation; 2.2 Basic Control Concepts; 2.3 Input-Output Representation; 2.4 Input-Output Linear Systems; 2.5 Loop Shaping of Linear Control Systems; 2.6 State-Space Representation; 2.7 Stochastic Systems; 2.8 Optimal Control
4.3 Active Suppression of Single Degree-of-Freedom Flutter4.4 Active Flutter Suppression of Typical Section; 4.5 Linear Feedback Stabilization; 4.6 Active Flutter Suppression of Three-Dimensional Wings; References; Chapter 5: Self-Tuning Regulation; 5.1 Introduction; 5.2 Online Plant Identification; 5.3 Design Methods for Stochastic Self-Tuning Regulators; 5.4 Aeroservoelastic Applications; References; Chapter 6: Nonlinear Systems Analysis and Design; 6.1 Introduction; 6.2 Preliminaries; 6.3 Stability in the Sense of Lyapunov; 6.4 Input-Output Stability; 6.5 Passivity; References
Chapter 7: Nonlinear Oscillatory Systems and Describing Functions7.1 Introduction; 7.2 Absolute Stability; 7.3 Describing Function Approximation; 7.4 Applications to Aeroservoelastic Systems; References; Chapter 8: Model Reference Adaptation of Aeroservoelastic Systems; 8.1 Lyapunov-Like Stability of Non-autonomous Systems; 8.2 Gradient-Based Adaptation; 8.3 Lyapunov-Based Adaptation; 8.4 Aeroservoelastic Applications; References; Chapter 9: Adaptive Backstepping Control; 9.1 Introduction; 9.2 Integrator Backstepping; 9.3 Aeroservoelastic Application; Reference
Chapter 10: Adaptive Control of Uncertain Nonlinear Systems10.1 Introduction; 10.2 Integral Adaptation; 10.3 Model Reference Adaptation of Nonlinear Plant; 10.4 Robust Model Reference Adaptation; References; Chapter 11: Adaptive Transonic Aeroservoelasticity; 11.1 Steady Transonic Flow Characteristics; 11.2 Unsteady Transonic Flow Characteristics; 11.3 Modelling for Transonic Unsteady Aerodynamics; 11.4 Transonic Aeroelastic Plant; 11.5 Adaptive Control of Control-Surface Nonlinearity; 11.6 Adaptive Control of Limit-Cycle Oscillation; References
Appendix A: Analytical Solution for Ideal Unsteady Aerodynamics
Record Nr. UNINA-9910137402703321
Tewari Ashish  
Chichester, England : , : Wiley, , 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Adaptive aeroservoelastic control / / Ashish Tewari
Adaptive aeroservoelastic control / / Ashish Tewari
Autore Tewari Ashish
Pubbl/distr/stampa Chichester, England : , : Wiley, , 2016
Descrizione fisica 1 online resource (482 p.)
Disciplina 629.132/6
Collana Aerospace Series
Soggetto topico Airplanes - Control systems
Aeroservoelasticity
Adaptive control systems
ISBN 1-118-92773-7
1-118-92772-9
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Aerospace Series List; Title Page; Copyright; Dedication; Table of Contents; About the Author; Series Editor's Preface; Preface; Chapter 1: Introduction; 1.1 Aeroservoelasticity; 1.2 Unsteady Aerodynamics; 1.3 Linear Feedback Design; 1.4 Parametric Uncertainty and Variation; 1.5 Adaptive Control Design; 1.6 Organization; References; Chapter 2: Linear Control Systems; 2.1 Notation; 2.2 Basic Control Concepts; 2.3 Input-Output Representation; 2.4 Input-Output Linear Systems; 2.5 Loop Shaping of Linear Control Systems; 2.6 State-Space Representation; 2.7 Stochastic Systems; 2.8 Optimal Control
4.3 Active Suppression of Single Degree-of-Freedom Flutter4.4 Active Flutter Suppression of Typical Section; 4.5 Linear Feedback Stabilization; 4.6 Active Flutter Suppression of Three-Dimensional Wings; References; Chapter 5: Self-Tuning Regulation; 5.1 Introduction; 5.2 Online Plant Identification; 5.3 Design Methods for Stochastic Self-Tuning Regulators; 5.4 Aeroservoelastic Applications; References; Chapter 6: Nonlinear Systems Analysis and Design; 6.1 Introduction; 6.2 Preliminaries; 6.3 Stability in the Sense of Lyapunov; 6.4 Input-Output Stability; 6.5 Passivity; References
Chapter 7: Nonlinear Oscillatory Systems and Describing Functions7.1 Introduction; 7.2 Absolute Stability; 7.3 Describing Function Approximation; 7.4 Applications to Aeroservoelastic Systems; References; Chapter 8: Model Reference Adaptation of Aeroservoelastic Systems; 8.1 Lyapunov-Like Stability of Non-autonomous Systems; 8.2 Gradient-Based Adaptation; 8.3 Lyapunov-Based Adaptation; 8.4 Aeroservoelastic Applications; References; Chapter 9: Adaptive Backstepping Control; 9.1 Introduction; 9.2 Integrator Backstepping; 9.3 Aeroservoelastic Application; Reference
Chapter 10: Adaptive Control of Uncertain Nonlinear Systems10.1 Introduction; 10.2 Integral Adaptation; 10.3 Model Reference Adaptation of Nonlinear Plant; 10.4 Robust Model Reference Adaptation; References; Chapter 11: Adaptive Transonic Aeroservoelasticity; 11.1 Steady Transonic Flow Characteristics; 11.2 Unsteady Transonic Flow Characteristics; 11.3 Modelling for Transonic Unsteady Aerodynamics; 11.4 Transonic Aeroelastic Plant; 11.5 Adaptive Control of Control-Surface Nonlinearity; 11.6 Adaptive Control of Limit-Cycle Oscillation; References
Appendix A: Analytical Solution for Ideal Unsteady Aerodynamics
Record Nr. UNINA-9910815180303321
Tewari Ashish  
Chichester, England : , : Wiley, , 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Automatic control in aerospace : Aerospace Control '94 : a postprint volume from the IFAC symposium, Palo Alto, California, USA, 12-16 September 1994 / / edited by D. B. Schaechter and K. R. Lorell
Automatic control in aerospace : Aerospace Control '94 : a postprint volume from the IFAC symposium, Palo Alto, California, USA, 12-16 September 1994 / / edited by D. B. Schaechter and K. R. Lorell
Edizione [First edition.]
Pubbl/distr/stampa Oxford, England : , : Pergamon, , 1995
Descrizione fisica 1 online resource (447 p.)
Disciplina 629.132/6
629.1326
Collana IFAC Postprint Volume
Soggetto topico Airplanes - Control systems
Airplanes - Automatic control
Space vehicles - Control systems
Space vehicles - Automatic control
ISBN 1-4832-9692-X
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Front Cover""; ""Automatic Control in Aerospace (Aerospace Control '94)""; ""Copyright Page""; ""Table of Contents""; ""IFAC SYMPOSIUM ON AUTOMATIC CONTROL IN AEROSPACE 1994""; ""CHAPTER 1. OPTIMAL MULTI-CRITERIA AEROASSISTED ORBITAL TRANSFER TRAJECTORIES""; ""1. INTRODUCTION""; ""2. MATHEMATICAL MODEL""; ""3. MULTI-CRITERIA TRAJECTORY OPTIMIZATION""; ""4. THE AEROASSISTED ORBITAL TRANSFER PROBLEM""; ""5. RESULTS AND DISCUSSION""; ""6. CONCLUSIONS""; ""Acknowledgments""; ""7. REFERENCES""; ""CHAPTER 2. ROCKET ASCENT WITH HEAT-FLUX AND SPLASH DOWNCONSTRAINTS""; ""1 INTRODUCTION""
""2 MATHEMATICAL MODELS""""3 OPTIMIZATION METHOD""; ""4 COMPUTATIONAL STUDY""; ""5 CONCLUSIONS""; ""6 REFERENCES""; ""CHAPTER 3. HIERARCHICAL MODELING APPROACH IN AIRCRAFT TRAJECTORY OPTIMIZATION""; ""1. INTRODUCTION""; ""2. MATHEMATICAL MODELING""; ""3. DYNAMIC-MODEL STRUCTURE""; ""4. HIERARCHICAL OPTIMIZATION""; ""5. NUMERICAL RESULTS""; ""CONCLUSIONS""; ""ACKNOWLEDGEMENTS""; ""REFERENCES""; ""CHAPTER 4. NONLINEAR ANALYSIS AND DESIGN OF SHUTTLE-TYPE ENTRY GUIDANCE""; ""1. INTRODUCTION""; ""2. GUIDANCE PROBLEM FORMULATION""; ""3. GUIDANCE LAWS""; ""4. STABILITY AND PERFORMANCE""
""5. ASSESSMENT""""6. CONCLUSIONS""; ""7. ACKNOWLEDGMENT""; ""8. REFERENCES""; ""CHAPTER 5. OPTIMAL GUIDANCE OF A SOLAR SAIL SPACECRAFT TO THE SUN-EARTH L2 POINT""; ""1. INTRODUCTION""; ""2. PROBLEM DEFINITION""; ""3. OPEN-LOOP TRAJECTORY""; ""4. GUIDANCE""; ""5. CONCLUSIONS""; ""6. REFERENCES""; ""CHAPTER 6. ADAPTIVE WING CAMBER OPTIMIZATION: A PERIODIC PERTURBATION APPROACH""; ""1. INTRODUCTION""; ""2. PROBLEM FORMULATION""; ""3. A PERIODIC PERTURBATION EXTREMASEARCHING TECHNIQUE: THE WORKING PRINCIPLE""; ""4. PRACTICAL IMPLEMENTATION OF THE ALGORITHM: EQUIVALENT CIRCUIT AND DESIGN""
""5. APPLICATION TO ACTIVE CAMBER OPTIMIZATION""""6. CONCLUDING REMARKS""; ""7. REFERENCES""; ""CHAPTER 7. PARAMETER ROBUST FLIGHT CONTROL SYSTEMFOR A FLEXIBLE AIRCRAFT""; ""1. INTRODUCTION""; ""2. MIXED CONTROL""; ""3. PARAMETER ROBUST MIXED CONTROL""; ""4. PERFORMANCE REQUIREMENT""; ""5. APPLICATION""; ""6. CONCLUSION""; ""7. REFERENCES""; ""CHAPTER 8. NON-SMOOTH RESONANCE CONTROL OF COMPLEX BIFURCATIONS IN AIRCRAFT FLIGHT""; ""1. INTRODUCTION""; ""2. NORMAL FORMS AND AVERAGING REDUCTION METHODS""; ""3. ESTIMATION OF RESIDUAL TERMS""; ""4 . RESONANCE STABILIZATION""
""5. ANALYSIS AND CONTROL OF COMPLEX BIFURCATIONS OF AN AIRCRAFT MODEL""""6. CONCLUSION""; ""7. REFERENCES""; ""CHAPTER 9. HIGH ANGLE OF ATTACK VELOCITY VECTOR ROLLS""; ""1. INTRODUCTION""; ""2. APPROACH""; ""3. MODELING""; ""4. QFT OVERVIEW""; ""5. ATTACK ON NONLINEARITIES AND UNCERTAINTY""; ""6. CONTROLLER DESIGN""; ""7. RESULTS""; ""8. CONCLUSIONS""; ""9. REFERENCES""; ""CHAPTER 10. A ROUTE ORIENTED PLANNING AND CONTROL CONCEPT FOR EFFICIENT FLIGHT OPERATIONS AT BUSY AIRPORTS""; ""1. INTRODUCTION""; ""2. CURRENT AIRPORT OPERATIONS""; ""3. CONCEPT DESCRIPTION""; ""4. DESIGN ALGORITHMS""
""5. PLANNING OF LANDING SEQUENCES AND SCHEDULES""
Record Nr. UNINA-9910788199903321
Oxford, England : , : Pergamon, , 1995
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Automatic control in aerospace : Aerospace Control '94 : a postprint volume from the IFAC symposium, Palo Alto, California, USA, 12-16 September 1994 / / edited by D. B. Schaechter and K. R. Lorell
Automatic control in aerospace : Aerospace Control '94 : a postprint volume from the IFAC symposium, Palo Alto, California, USA, 12-16 September 1994 / / edited by D. B. Schaechter and K. R. Lorell
Edizione [First edition.]
Pubbl/distr/stampa Oxford, England : , : Pergamon, , 1995
Descrizione fisica 1 online resource (447 p.)
Disciplina 629.132/6
629.1326
Collana IFAC Postprint Volume
Soggetto topico Airplanes - Control systems
Airplanes - Automatic control
Space vehicles - Control systems
Space vehicles - Automatic control
ISBN 1-4832-9692-X
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Front Cover""; ""Automatic Control in Aerospace (Aerospace Control '94)""; ""Copyright Page""; ""Table of Contents""; ""IFAC SYMPOSIUM ON AUTOMATIC CONTROL IN AEROSPACE 1994""; ""CHAPTER 1. OPTIMAL MULTI-CRITERIA AEROASSISTED ORBITAL TRANSFER TRAJECTORIES""; ""1. INTRODUCTION""; ""2. MATHEMATICAL MODEL""; ""3. MULTI-CRITERIA TRAJECTORY OPTIMIZATION""; ""4. THE AEROASSISTED ORBITAL TRANSFER PROBLEM""; ""5. RESULTS AND DISCUSSION""; ""6. CONCLUSIONS""; ""Acknowledgments""; ""7. REFERENCES""; ""CHAPTER 2. ROCKET ASCENT WITH HEAT-FLUX AND SPLASH DOWNCONSTRAINTS""; ""1 INTRODUCTION""
""2 MATHEMATICAL MODELS""""3 OPTIMIZATION METHOD""; ""4 COMPUTATIONAL STUDY""; ""5 CONCLUSIONS""; ""6 REFERENCES""; ""CHAPTER 3. HIERARCHICAL MODELING APPROACH IN AIRCRAFT TRAJECTORY OPTIMIZATION""; ""1. INTRODUCTION""; ""2. MATHEMATICAL MODELING""; ""3. DYNAMIC-MODEL STRUCTURE""; ""4. HIERARCHICAL OPTIMIZATION""; ""5. NUMERICAL RESULTS""; ""CONCLUSIONS""; ""ACKNOWLEDGEMENTS""; ""REFERENCES""; ""CHAPTER 4. NONLINEAR ANALYSIS AND DESIGN OF SHUTTLE-TYPE ENTRY GUIDANCE""; ""1. INTRODUCTION""; ""2. GUIDANCE PROBLEM FORMULATION""; ""3. GUIDANCE LAWS""; ""4. STABILITY AND PERFORMANCE""
""5. ASSESSMENT""""6. CONCLUSIONS""; ""7. ACKNOWLEDGMENT""; ""8. REFERENCES""; ""CHAPTER 5. OPTIMAL GUIDANCE OF A SOLAR SAIL SPACECRAFT TO THE SUN-EARTH L2 POINT""; ""1. INTRODUCTION""; ""2. PROBLEM DEFINITION""; ""3. OPEN-LOOP TRAJECTORY""; ""4. GUIDANCE""; ""5. CONCLUSIONS""; ""6. REFERENCES""; ""CHAPTER 6. ADAPTIVE WING CAMBER OPTIMIZATION: A PERIODIC PERTURBATION APPROACH""; ""1. INTRODUCTION""; ""2. PROBLEM FORMULATION""; ""3. A PERIODIC PERTURBATION EXTREMASEARCHING TECHNIQUE: THE WORKING PRINCIPLE""; ""4. PRACTICAL IMPLEMENTATION OF THE ALGORITHM: EQUIVALENT CIRCUIT AND DESIGN""
""5. APPLICATION TO ACTIVE CAMBER OPTIMIZATION""""6. CONCLUDING REMARKS""; ""7. REFERENCES""; ""CHAPTER 7. PARAMETER ROBUST FLIGHT CONTROL SYSTEMFOR A FLEXIBLE AIRCRAFT""; ""1. INTRODUCTION""; ""2. MIXED CONTROL""; ""3. PARAMETER ROBUST MIXED CONTROL""; ""4. PERFORMANCE REQUIREMENT""; ""5. APPLICATION""; ""6. CONCLUSION""; ""7. REFERENCES""; ""CHAPTER 8. NON-SMOOTH RESONANCE CONTROL OF COMPLEX BIFURCATIONS IN AIRCRAFT FLIGHT""; ""1. INTRODUCTION""; ""2. NORMAL FORMS AND AVERAGING REDUCTION METHODS""; ""3. ESTIMATION OF RESIDUAL TERMS""; ""4 . RESONANCE STABILIZATION""
""5. ANALYSIS AND CONTROL OF COMPLEX BIFURCATIONS OF AN AIRCRAFT MODEL""""6. CONCLUSION""; ""7. REFERENCES""; ""CHAPTER 9. HIGH ANGLE OF ATTACK VELOCITY VECTOR ROLLS""; ""1. INTRODUCTION""; ""2. APPROACH""; ""3. MODELING""; ""4. QFT OVERVIEW""; ""5. ATTACK ON NONLINEARITIES AND UNCERTAINTY""; ""6. CONTROLLER DESIGN""; ""7. RESULTS""; ""8. CONCLUSIONS""; ""9. REFERENCES""; ""CHAPTER 10. A ROUTE ORIENTED PLANNING AND CONTROL CONCEPT FOR EFFICIENT FLIGHT OPERATIONS AT BUSY AIRPORTS""; ""1. INTRODUCTION""; ""2. CURRENT AIRPORT OPERATIONS""; ""3. CONCEPT DESCRIPTION""; ""4. DESIGN ALGORITHMS""
""5. PLANNING OF LANDING SEQUENCES AND SCHEDULES""
Record Nr. UNINA-9910808895403321
Oxford, England : , : Pergamon, , 1995
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Flight formation control [[electronic resource] /] / edited by Jose A. Guerrero, Rogelio Lozano
Flight formation control [[electronic resource] /] / edited by Jose A. Guerrero, Rogelio Lozano
Pubbl/distr/stampa London, : ISTE Ltd.
Descrizione fisica 1 online resource (342 p.)
Disciplina 629.132/6
Altri autori (Persone) GuerreroJose A <1977-> (Jose Alfredo)
LozanoR <1954-> (Rogelio)
Collana ISTE
Soggetto topico Airplanes - Control systems
Airplanes - Automatic control
Drone aircraft - Control systems
Drone aircraft - Automatic control
Stability of airplanes
ISBN 1-118-38719-8
1-299-18849-4
1-118-56325-5
1-118-56322-0
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover; Flight Formation Control; Title Page; Copyright Page; Table of Contents; Chapter 1. Introduction; 1.1. Motivation; 1.2. Historical background; 1.2.1. Aviation history; 1.2.2. Evolution of UAVs; 1.2.3. UAV classification; 1.3. Flight control; 1.4. Flight formation control; 1.4.1. Multiple-input and multiple-output; 1.4.2. Leader/follower; 1.4.3. Virtual structure; 1.4.4. Behavior-based control; 1.4.5. Passivity-based control; 1.5. Outline of the book; 1.6. Bibliography; Chapter 2. Theoretical Preliminaries; 2.1. Passivity; 2.2. Graph theory; 2.3. Robustness problems
2.3.1. Representation of the parametric uncertainty2.3.2. Families of polynomials; 2.4. Bibliography; Chapter 3. Multiagent Coordination Strategies; 3.1. Introduction; 3.2. Controllability and observability of interconnections; 3.2.1. Cyclic topology; 3.2.2. Chain topology: input and output on agent 1; 3.2.3. Chain topology: input and output on agent 2; 3.2.4. Eigenvalues and eigenvectors of the system; 3.2.5. General case; 3.2.6. The cyclic topology in the general case; 3.2.6.1. Observability; 3.2.6.2. Controllability; 3.2.7. The chain topology in the general case; 3.2.7.1. Controllability
3.2.7.2. Observability3.2.8. Combinations of chain and cyclic topologies; 3.2.8.1. Controllability; 3.2.8.2. Observability; 3.2.9. Simple configurations that are either non-controllable or non-observable; 3.2.9.1. Example 1; 3.2.9.2. Example 2; 3.2.9.3. Example 3; 3.2.9.4. Example 4; 3.2.9.5. Example 5; 3.3. Formation leader tracking; 3.3.1. Formation leader tracking in the general case; 3.3.2. Observer design; 3.3.3. Simulations; 3.4. Time-varying trajectory tracking; 3.5. Linear high-order multiagent consensus; 3.5.1. Trajectory-tracking control; 3.6. Conclusion; 3.7. Bibliography
Chapter 4. Robust Control Design of Multiagent Systems with Parametric Uncertainty4.1. Introduction; 4.2. Robust control design; 4.3. Robust stability analysis; 4.3.1. Robust strict positive realness; 4.3.2. Robust absolute stability; 4.4. Robust stability of time-delay systems; 4.5. Application to multiagent systems; 4.5.1. Cyclic topology; 4.5.2. Chain topology; 4.5.3. Balanced graph topology; 4.6. Conclusions; 4.7. Bibliography; Chapter 5. On Adaptive and Robust Controlled Synchronization of Networked Robotic Systems on Strongly Connected Graphs; 5.1. Summary; 5.2. Introduction
5.3. Problem formulation5.4. Adaptive controlled synchronization on strongly connected graphs; 5.4.1. Delay-free synchronization; 5.4.2. Synchronization with time delay; 5.5. Robust controlled synchronization on strongly connected graph; 5.5.1. Delay-free synchronization; 5.5.2. Synchronization with time delay; 5.6. Numerical examples; 5.6.1. Adaptive tracking algorithm; 5.6.2. Robust tracking algorithm; 5.6.3. Disturbances; 5.7. Conclusions; 5.8. Appendix; 5.8.1. Robotic system; 5.8.2. Graph theory; 5.9. Bibliography; Chapter 6. Modeling and Control of Mini UAV; 6.1. Introduction
6.2. General model
Record Nr. UNINA-9910141502903321
London, : ISTE Ltd.
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Flight formation control / / edited by Jose A. Guerrero, Rogelio Lozano
Flight formation control / / edited by Jose A. Guerrero, Rogelio Lozano
Edizione [1st ed.]
Pubbl/distr/stampa London, : ISTE Ltd.
Descrizione fisica 1 online resource (342 p.)
Disciplina 629.132/6
Altri autori (Persone) GuerreroJose A <1977-> (Jose Alfredo)
LozanoR <1954-> (Rogelio)
Collana ISTE
Soggetto topico Airplanes - Control systems
Airplanes - Automatic control
Drone aircraft - Control systems
Drone aircraft - Automatic control
Stability of airplanes
ISBN 1-118-38719-8
1-299-18849-4
1-118-56325-5
1-118-56322-0
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover; Flight Formation Control; Title Page; Copyright Page; Table of Contents; Chapter 1. Introduction; 1.1. Motivation; 1.2. Historical background; 1.2.1. Aviation history; 1.2.2. Evolution of UAVs; 1.2.3. UAV classification; 1.3. Flight control; 1.4. Flight formation control; 1.4.1. Multiple-input and multiple-output; 1.4.2. Leader/follower; 1.4.3. Virtual structure; 1.4.4. Behavior-based control; 1.4.5. Passivity-based control; 1.5. Outline of the book; 1.6. Bibliography; Chapter 2. Theoretical Preliminaries; 2.1. Passivity; 2.2. Graph theory; 2.3. Robustness problems
2.3.1. Representation of the parametric uncertainty2.3.2. Families of polynomials; 2.4. Bibliography; Chapter 3. Multiagent Coordination Strategies; 3.1. Introduction; 3.2. Controllability and observability of interconnections; 3.2.1. Cyclic topology; 3.2.2. Chain topology: input and output on agent 1; 3.2.3. Chain topology: input and output on agent 2; 3.2.4. Eigenvalues and eigenvectors of the system; 3.2.5. General case; 3.2.6. The cyclic topology in the general case; 3.2.6.1. Observability; 3.2.6.2. Controllability; 3.2.7. The chain topology in the general case; 3.2.7.1. Controllability
3.2.7.2. Observability3.2.8. Combinations of chain and cyclic topologies; 3.2.8.1. Controllability; 3.2.8.2. Observability; 3.2.9. Simple configurations that are either non-controllable or non-observable; 3.2.9.1. Example 1; 3.2.9.2. Example 2; 3.2.9.3. Example 3; 3.2.9.4. Example 4; 3.2.9.5. Example 5; 3.3. Formation leader tracking; 3.3.1. Formation leader tracking in the general case; 3.3.2. Observer design; 3.3.3. Simulations; 3.4. Time-varying trajectory tracking; 3.5. Linear high-order multiagent consensus; 3.5.1. Trajectory-tracking control; 3.6. Conclusion; 3.7. Bibliography
Chapter 4. Robust Control Design of Multiagent Systems with Parametric Uncertainty4.1. Introduction; 4.2. Robust control design; 4.3. Robust stability analysis; 4.3.1. Robust strict positive realness; 4.3.2. Robust absolute stability; 4.4. Robust stability of time-delay systems; 4.5. Application to multiagent systems; 4.5.1. Cyclic topology; 4.5.2. Chain topology; 4.5.3. Balanced graph topology; 4.6. Conclusions; 4.7. Bibliography; Chapter 5. On Adaptive and Robust Controlled Synchronization of Networked Robotic Systems on Strongly Connected Graphs; 5.1. Summary; 5.2. Introduction
5.3. Problem formulation5.4. Adaptive controlled synchronization on strongly connected graphs; 5.4.1. Delay-free synchronization; 5.4.2. Synchronization with time delay; 5.5. Robust controlled synchronization on strongly connected graph; 5.5.1. Delay-free synchronization; 5.5.2. Synchronization with time delay; 5.6. Numerical examples; 5.6.1. Adaptive tracking algorithm; 5.6.2. Robust tracking algorithm; 5.6.3. Disturbances; 5.7. Conclusions; 5.8. Appendix; 5.8.1. Robotic system; 5.8.2. Graph theory; 5.9. Bibliography; Chapter 6. Modeling and Control of Mini UAV; 6.1. Introduction
6.2. General model
Record Nr. UNINA-9910827582003321
London, : ISTE Ltd.
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Motion coordination for VTOL unmanned aerial vehicles : attitude synchronisation and formation control / / Abdelkader Abdessameud, Abdelhamid Tayebi
Motion coordination for VTOL unmanned aerial vehicles : attitude synchronisation and formation control / / Abdelkader Abdessameud, Abdelhamid Tayebi
Autore Abdessameud Abdelkader
Edizione [1st ed. 2013.]
Pubbl/distr/stampa New York, : Springer, 2013
Descrizione fisica 1 online resource (xv, 182 pages) : illustrations (some color)
Disciplina 623
629.132/6
629.1326
Altri autori (Persone) TayebiAbdelhamid
Collana Advances in industrial control
Soggetto topico Drone aircraft - Control systems
Aeronautics
ISBN 1-4471-5094-5
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Background and Preliminaries -- Mathematical Models of Flying Vehicles -- Attitude Synchronization -- Attitude Synchronization with Communication Delays -- Global Trajectory Tracking of VTOL UAVs -- Formation Control of VTOL UAVs -- Formation Control with Communication Delays.
Record Nr. UNINA-9910741179703321
Abdessameud Abdelkader  
New York, : Springer, 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Optimal control theory with aerospace applications [[electronic resource] /] / Joseph Z. Ben-Asher
Optimal control theory with aerospace applications [[electronic resource] /] / Joseph Z. Ben-Asher
Autore Ben-Asher Joseph Z. <1955->
Pubbl/distr/stampa Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2010
Descrizione fisica xvii, 262 p. : ill
Disciplina 629.132/6
Collana AIAA education series
Soggetto topico Automatic pilot (Airplanes)
Flight control
Guided missiles - Control systems
Soggetto genere / forma Electronic books.
ISBN 1-60086-734-0
1-60086-733-2
1-61344-043-X
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Historical background -- Ordinary minimum problems : from the beginning of calculus to Kuhn-Tucker -- Calculus of variations : from Bernoulli to Bliss -- Minimum principle of Pontryagin and Hestenes -- Application of the Jacobi test in optimal control and neighboring extremals -- Numerical techniques for the optimal control problem -- Singular perturbation technique and its application to air-to-space interception -- Application to aircraft performance : Rutowski and Kaiser's techniques and more -- Application to rocket performance : the Goddard problem -- Application to missile guidance : proportional navigation -- Application to time-optimal rotational maneuvers of flexible spacecraft.
Record Nr. UNINA-9910465013703321
Ben-Asher Joseph Z. <1955->  
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2010
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Optimal control theory with aerospace applications [[electronic resource] /] / Joseph Z. Ben-Asher
Optimal control theory with aerospace applications [[electronic resource] /] / Joseph Z. Ben-Asher
Autore Ben-Asher Joseph Z. <1955->
Pubbl/distr/stampa Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2010
Descrizione fisica xvii, 262 p. : ill
Disciplina 629.132/6
Collana AIAA education series
Soggetto topico Automatic pilot (Airplanes)
Flight control
Guided missiles - Control systems
ISBN 1-60086-734-0
1-60086-733-2
1-61344-043-X
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Historical background -- Ordinary minimum problems : from the beginning of calculus to Kuhn-Tucker -- Calculus of variations : from Bernoulli to Bliss -- Minimum principle of Pontryagin and Hestenes -- Application of the Jacobi test in optimal control and neighboring extremals -- Numerical techniques for the optimal control problem -- Singular perturbation technique and its application to air-to-space interception -- Application to aircraft performance : Rutowski and Kaiser's techniques and more -- Application to rocket performance : the Goddard problem -- Application to missile guidance : proportional navigation -- Application to time-optimal rotational maneuvers of flexible spacecraft.
Record Nr. UNINA-9910789085103321
Ben-Asher Joseph Z. <1955->  
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2010
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Optimal control theory with aerospace applications [[electronic resource] /] / Joseph Z. Ben-Asher
Optimal control theory with aerospace applications [[electronic resource] /] / Joseph Z. Ben-Asher
Autore Ben-Asher Joseph Z. <1955->
Pubbl/distr/stampa Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2010
Descrizione fisica xvii, 262 p. : ill
Disciplina 629.132/6
Collana AIAA education series
Soggetto topico Automatic pilot (Airplanes)
Flight control
Guided missiles - Control systems
ISBN 1-60086-734-0
1-60086-733-2
1-61344-043-X
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Historical background -- Ordinary minimum problems : from the beginning of calculus to Kuhn-Tucker -- Calculus of variations : from Bernoulli to Bliss -- Minimum principle of Pontryagin and Hestenes -- Application of the Jacobi test in optimal control and neighboring extremals -- Numerical techniques for the optimal control problem -- Singular perturbation technique and its application to air-to-space interception -- Application to aircraft performance : Rutowski and Kaiser's techniques and more -- Application to rocket performance : the Goddard problem -- Application to missile guidance : proportional navigation -- Application to time-optimal rotational maneuvers of flexible spacecraft.
Record Nr. UNINA-9910824305503321
Ben-Asher Joseph Z. <1955->  
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2010
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui