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Biblioteca

MARC Lista (tabellare)
Advances in spacecraft attitude control / / edited by Timothy Sands
Advances in spacecraft attitude control / / edited by Timothy Sands
Pubbl/distr/stampa London, England : , : IntechOpen, , [2020]
Descrizione fisica 1 online resource (284 pages) : illustrations
Disciplina 629.4742
Soggetto topico Space vehicles - Attitude control systems
Space vehicles - Dynamics
Astrodynamics
ISBN 1-78984-803-2
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910407750203321
London, England : , : IntechOpen, , [2020]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Chaos in attitude dynamics of spacecraft / / by Yanzhu Liu, Liqun Chen
Chaos in attitude dynamics of spacecraft / / by Yanzhu Liu, Liqun Chen
Autore Liu Yanzhu
Edizione [1st ed. 2013.]
Pubbl/distr/stampa Beijing, : Tsinghua University Press
Descrizione fisica 1 online resource (174 p.)
Disciplina 629.4742
Altri autori (Persone) ChenLiqun
Collana Tsinghua University Lecture Notes
Soggetto topico Space vehicles - Attitude control systems
Space vehicles - Dynamics
Astrodynamics
ISBN 3-642-30080-4
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Primer on Spacecraft Dynamics -- A Survey of Chaos Theory -- Chaos in Planar Attitude Motion of Spacecraft -- Chaos in Spatial Attitude Motion of Spacecraft -- Control of Chaotic Attitude Motion.
Record Nr. UNINA-9910438060503321
Liu Yanzhu  
Beijing, : Tsinghua University Press
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Control allocation for spacecraft under actuator faults / / Qinglei Hu [et al.]
Control allocation for spacecraft under actuator faults / / Qinglei Hu [et al.]
Autore Hu Qinglei
Pubbl/distr/stampa Singapore : , : Springer, , [2021]
Descrizione fisica 1 online resource (xviii, 221 pages)
Disciplina 629.4742
Soggetto topico Space vehicles - Attitude control systems
Actuators
Vehicles espacials
Actuadors
Sistemes adaptatius
Soggetto genere / forma Llibres electrònics
ISBN 981-16-0439-8
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Intro -- Preface -- Acknowledgements -- Contents -- Acronyms -- 1 Introduction -- 1.1 Background and Motivations -- 1.2 Introduction to Control Allocation -- 1.2.1 Control Allocation Methods -- 1.2.2 Applications of Control Allocation in Aeronautics and Astronautics -- 1.3 Introduction to Fault-Tolerant Control -- 1.3.1 Fault-Tolerant Control Methods -- 1.3.2 Applications of Fault-Tolerant Control in Aeronautics and Astronautics -- 1.4 Organization of the Book -- References -- 2 Mathematical Model of the Attitude Control System -- 2.1 Spacecraft Attitude Kinematics -- 2.1.1 Euler Angles Based Model -- 2.1.2 Quaternion Based Model -- 2.1.3 Modified Rodrigues Parameters Based Model -- 2.2 Spacecraft Attitude Dynamics Model -- References -- 3 Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization -- 3.1 Introduction -- 3.2 Problem Formulation -- 3.2.1 Spacecraft Attitude Dynamics -- 3.2.2 Control Objective -- 3.3 Attitude Control Law Design -- 3.3.1 SPD-Based Virtual/Baseline Control Law Design -- 3.3.2 Null-Space-Based Optimal Control Reallocation Scheme -- 3.4 Simulation Results -- 3.4.1 Time Response Results Under the Proposed Control Law -- 3.4.2 Energy Consumption Analysis -- 3.5 Conclusions -- References -- 4 Robust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment -- 4.1 Introduction -- 4.2 Problem Formulation -- 4.2.1 Actuator Configuration with Misalignment -- 4.2.2 Control Objective -- 4.3 Control Law Design -- 4.3.1 Nonsingular Terminal Sliding Mode Based Virtual Finite Time Feedback Controller Design -- 4.3.2 Robust Least Squares-Based Control Allocator Design Under Actuator Misalignment -- 4.4 Simulation Results -- 4.4.1 Simulation Results with Misalignment -- 4.4.2 Energy Consumption Analysis -- 4.5 Conclusions -- References.
5 Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation -- 5.1 Introduction -- 5.2 Problem Formulation -- 5.2.1 Definitions and Lemmas -- 5.3 Saturated Finite-Time Fault-Tolerant Control Law Design -- 5.3.1 Novel Time-Varying Terminal Sliding Mode Design -- 5.3.2 Basic Saturated Finite-Time Controller Design -- 5.3.3 Saturated Fault-Tolerant Finite-Time Controller Design -- 5.3.4 The Advantage of Modification Matrix A -- 5.4 Simulation Results -- 5.5 Conclusions -- References -- 6 Extended State Observer Based Optimal Attitude Robust Control of Spacecraft -- 6.1 Introduction -- 6.2 Problem Formulation -- 6.3 Robust Optimal Attitude Controller Design -- 6.3.1 Extended State Observer Design -- 6.3.2 Inverse Optimal Controller Design with Uncertainties -- 6.3.3 CLF and Zero Dynamics Based Optimal Controller Design -- 6.4 Simulation Results -- 6.4.1 Comparison and Analysis Under Different Controllers -- 6.4.2 Comparisons and Analyses of Energy Consumptions Under Different Controllers -- 6.5 Conclusions -- References -- 7 Spacecraft Attitude Fault-Tolerant Control Based on Iterative Learning Observer and Control Allocation -- 7.1 Introduction -- 7.2 Problem Formulation -- 7.3 Iterative Learning Observer Design -- 7.4 Control Strategy Design -- 7.4.1 Virtual Feedback Controller Design -- 7.4.2 Robust Control Allocation Design -- 7.5 Simulation Results -- 7.5.1 Case 1 -- 7.5.2 Case 2 -- 7.6 Conclusions -- References -- 8 Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft -- 8.1 Introduction -- 8.2 Problem Formulation -- 8.3 Attitude Control Law Design -- 8.3.1 SPD-based Virtual/Baseline Control Law Design -- 8.3.2 A Closed-Loop Control Allocation Design with Optimization Method -- 8.4 Simulation Results -- 8.4.1 Attitude Control without Actuator Uncertainties and Disturbances.
8.4.2 Attitude Control with Actuator Uncertainties and Disturbances -- 8.5 Conclusions -- References -- 9 Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults -- 9.1 Introduction -- 9.2 Problem Formulation -- 9.2.1 System Schematic Diagram -- 9.2.2 Problem Formulation -- 9.3 Control Scheme Design and Stability Analysis -- 9.3.1 Baseline Control Law Design -- 9.3.2 Online Robust Control Allocation Design -- 9.3.3 Online Pseudo-Inverse Control Allocation -- 9.3.4 Closed-Loop Stability with Online Control Allocation Analysis -- 9.4 Simulation Results -- 9.4.1 Performance with FDD Estimation Uncertainty Bound η= 5% -- 9.4.2 Performance with FDD Estimation Uncertainty Bound η=33% -- 9.5 Conclusions -- References -- 10 Conclusions -- 10.1 Conclusions -- 10.2 Open Problems and Challenges.
Record Nr. UNINA-9910739412403321
Hu Qinglei  
Singapore : , : Springer, , [2021]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Fundamentals of Spacecraft Attitude Determination and Control / / by F. Landis Markley, John L. Crassidis
Fundamentals of Spacecraft Attitude Determination and Control / / by F. Landis Markley, John L. Crassidis
Autore Markley F. Landis
Edizione [1st ed. 2014.]
Pubbl/distr/stampa New York, NY : , : Springer New York : , : Imprint : Springer, , 2014
Descrizione fisica 1 online resource (XVI, 470 p. 96 illus., 4 illus. in color.)
Disciplina 629.4742
Collana Space Technology Library
Soggetto topico Aerospace engineering
Astronautics
Dynamics
Ergodic theory
Automatic control
Aerospace Technology and Astronautics
Dynamical Systems and Ergodic Theory
Control and Systems Theory
ISBN 1-4939-0802-2
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Attitude Determination and Estimation -- Matrices, Vectors, Frames, Transforms -- Rotational Kinematics and Dynamics -- Sensors and Actuators -- Static Attitude Determination Methods -- Filtering for Attitude Determination -- Attitude Control.
Record Nr. UNINA-9910299748103321
Markley F. Landis  
New York, NY : , : Springer New York : , : Imprint : Springer, , 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Inertial navigation / Richard H. Parvin ; contributing authors William E. Shephard, W. Bruce Walker, David W. Geyer
Inertial navigation / Richard H. Parvin ; contributing authors William E. Shephard, W. Bruce Walker, David W. Geyer
Autore Parvin, Richard H.
Pubbl/distr/stampa Princeton ; Toronto ; New York ; London : Van Nostrand, 1962
Descrizione fisica XXI, 370 p. : ill. ; 24 cm
Disciplina 629.4742
Collana Principles of guided missile design
Soggetto non controllato Navigazione inerziale
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNIPARTHENOPE-000010294
Parvin, Richard H.  
Princeton ; Toronto ; New York ; London : Van Nostrand, 1962
Materiale a stampa
Lo trovi qui: Univ. Parthenope
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Optimal Space Flight Navigation : An Analytical Approach / / by Ashish Tewari
Optimal Space Flight Navigation : An Analytical Approach / / by Ashish Tewari
Autore Tewari Ashish
Edizione [1st ed. 2019.]
Pubbl/distr/stampa Cham : , : Springer International Publishing : , : Imprint : Birkhäuser, , 2019
Descrizione fisica 1 online resource (277 pages)
Disciplina 629.4742
Collana Control Engineering
Soggetto topico System theory
Automatic control
Calculus of variations
Aerospace engineering
Astronautics
Systems Theory, Control
Control and Systems Theory
Calculus of Variations and Optimal Control; Optimization
Aerospace Technology and Astronautics
ISBN 3-030-03789-4
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto 1. Introduction -- 2. Analytical Optimal Control -- 3. Orbital Mechanics and Impulsive Transfer -- 4. Two-Body Maneuvers with Unbounded Continuous Inputs -- 5. Optimal Maneuvers with Bounded Inputs -- 6. Flight in Non-spherical Gravity Fields.
Record Nr. UNINA-9910337654603321
Tewari Ashish  
Cham : , : Springer International Publishing : , : Imprint : Birkhäuser, , 2019
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters / / Jie Wang, Dong-Xu Li
Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters / / Jie Wang, Dong-Xu Li
Autore Wang Jie <1275-1336, >
Pubbl/distr/stampa Singapore : , : Springer, , [2022]
Descrizione fisica 1 online resource (190 pages)
Disciplina 629.4742
Soggetto topico Space vehicles - Attitude control systems
Stability of space vehicles
ISBN 981-16-5097-7
981-16-5096-9
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910743364903321
Wang Jie <1275-1336, >  
Singapore : , : Springer, , [2022]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Spacecraft attitude determination and control / written by Members of the technical staff Attitude Systems Operation, Computer Sciences Corporation ; edited by James R. Wertz
Spacecraft attitude determination and control / written by Members of the technical staff Attitude Systems Operation, Computer Sciences Corporation ; edited by James R. Wertz
Autore Computer Sciences Corporation : Attitude Systems Operation
Pubbl/distr/stampa Dordrecht [etc.], : Kluwer Academic, c1978
Descrizione fisica XVI, 858 p. : ill. ; 25 cm
Disciplina 629.47
629.4742
Collana Astrophysics and space science library
Soggetto topico Aeronautica
VEICOLI SPAZIALI - STRUMENTI DI CONTROLLO
ISBN 9027709599
9027712042
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNISANNIO-AQ10008139
Computer Sciences Corporation : Attitude Systems Operation  
Dordrecht [etc.], : Kluwer Academic, c1978
Materiale a stampa
Lo trovi qui: Univ. del Sannio
Opac: Controlla la disponibilità qui
Spacecraft Attitude Dynamics
Spacecraft Attitude Dynamics
Autore Hughes Peter C
Edizione [1st ed.]
Pubbl/distr/stampa Newburyport, : Dover Publications, 2012
Descrizione fisica 1 online resource (1137 p.)
Disciplina 629.4742
Collana Dover Books on Aeronautical Engineering
Soggetto topico Space vehicles - Attitude control systems
ISBN 0-486-14013-X
1-62198-601-2
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto 3.7 Dynamics of a System of Rigid Bodies3.8 Problems; Chapter 4 Attitude Dynamics of a Rigid Body; 4.1 Basic Motion Equations; 4.2 Torque-Free Motion; Ŕ Inertially Axisymmetrical; 4.3 Torque-Free Motion; Ŕ Tri-inertial; 4.4 Stability of Motion for Ŕ; 4.5 Motion of a Rigid Body Under Torque; 4.6 Problems; Chapter 5 Effect of Internal Energy Dissipation on the Directional Stability of Spinning Bodies; 5.1 Quasi-Rigid Body with an Energy Sink, Ŕ; 5.2 Rigid Body with a Point Mass Damper, Ŕ + Ŕ; 5.3 Problems; Chapter 6 Directional Stability of Multispin Vehicles; 6.1 The Ŕ + Ŵ Gyrostat
6.2 Gyrostat with Nonspinning Carrier6.3 The Zero Momentum Gyrostat; 6.4 The General Case; 6.5 System of Coaxial Wheels; 6.6 Problems; Chapter 7 Effect of Internal Energy Dissipation on the Directional Stability of Gyrostats; 7.1 Energy Sink Analyses; 7.2 Gyrostats with Discrete Dampers; 7.3 Problems; Chapter 8 Spacecraft Torques; 8.1 Gravitational Torque; 8.2 Aerodynamic Torque; 8.3 Radiation Torques; 8.4 Other Environmental Torques; 8.5 Nonenvironmental Torques; 8.6 Closing Remarks; 8.7 Problems; Chapter 9 Gravitational Stabilization; 9.1 Context
9.2 Equilibria for a Rigid Body in a Circular Orbit9.3 Design of Gravitationally Stabilized Satellites; 9.4 Flight Experience; 9.5 Problems; Chapter 10 Spin Stabilization in Orbit; 10.1 Spinning Rigid Body in Orbit; 10.2 Design of Spin-Stabilized Satellites; 10.3 Long-Term Effects of Environmental Torques, and Flight Data; 10.4 Problems; Chapter 11 Dual-Stabilization in Orbit: Gyrostats and Bias Momentum Satellites; 11.1 The Gyrostat in Orbit; 11.2 Gyrostats with External Rotors; 11.3 Bias Momentum Satellites; 11.4 Problems; Appendix A Elements of Stability Theory; A.1 Stability Definitions
A.2 Stability of the OriginA.3 The Linear Approximation; A.4 Nonlinear Inferences from Infinitesimal Stability Properties; A.5 Liapunov's Method; A.6 Stability of Linear Stationary Mechanical Systems; A.7 Stability Ideas Specialized to Attitude Dynamics; Appendix B Vectrices; B.1 Remarks on Terminology; B.2 Vectrices; B.3 Several Reference Frames; B.4 Kinematics of Vectrices; B.5 Derivative with Respect to a Vector; Appendix C List of Symbols; C.1 Lowercase Symbols; C.2 Uppercase Symbols; C.3 Lowercase Greek Symbols; C.4 Uppercase Greek Symbols; C.5 Other Notational Conventions; References
Errata
Record Nr. UNINA-9911006598703321
Hughes Peter C  
Newburyport, : Dover Publications, 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Spacecraft Collision Avoidance Technology / / Rongzhi, Zhang [and others]
Spacecraft Collision Avoidance Technology / / Rongzhi, Zhang [and others]
Autore Rongzhi Zhang
Pubbl/distr/stampa San Diego, CA, USA, : Elsevier Science, 2020
Descrizione fisica 1 online resource
Disciplina 629.4742
Altri autori (Persone) KaizhongYang
Soggetto topico Space vehicle accidents
Space vehicles
ISBN 9780128182413
0128182415
9780128180112
0128180110
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9911007197503321
Rongzhi Zhang  
San Diego, CA, USA, : Elsevier Science, 2020
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui