08712nam 2200505 450 991075408760332120231104192644.0981-9946-53-0(MiAaPQ)EBC30806120(Au-PeEL)EBL30806120(PPN)272919705(EXLCZ)992854003030004120231104d2023 uy 0engurcnu||||||||txtrdacontentcrdamediacrrdacarrierSpacecraft Maneuver with Performance Guaranteed Control, Games, and Cooperation /Yufeng Gao and Dongyu LiFirst edition.Singapore :Springer Nature Singapore Pte Ltd.,[2023]©20231 online resource (452 pages)Print version: Gao, Yufeng Spacecraft Maneuver with Performance Guaranteed Singapore : Springer,c2023 9789819946525 Includes bibliographical references.Intro -- Preface -- Contents -- 1 Introduction -- 1.1 Research Background -- 1.2 On-Orbit Service Spacecraft Control -- 1.2.1 On-Orbit Service Spacecraft -- 1.2.2 Spacecraft Relative Motion Control -- 1.2.3 Spacecraft Constraint Control -- 1.2.4 Spacecraft Optimal Control -- 1.2.5 Spacecraft Differential Games -- 1.2.6 Spacecraft Cooperation -- 1.3 Performance Guaranteed Control -- 1.3.1 Problem Formulation of Performance Guaranteed Control -- 1.3.2 Performance Constraint Control with Constant Value Constraints -- 1.3.3 Funnel Control -- 1.3.4 Prescribed Performance Control -- 1.3.5 Finite-Time Prescribed Performance Control -- 1.3.6 Performance Guaranteed Control for Spacecraft -- 1.4 Main Contents of This Book -- References -- 2 Spacecraft Model and Preliminaries -- 2.1 Introduction -- 2.2 Coordinate Systems -- 2.3 Spacecraft Systems -- 2.3.1 Quaternion -- 2.3.2 Spacecraft Attitude Systems -- 2.3.3 Spacecraft Formation Systems -- 2.4 Relevant Knowledge of Nonlinear System Control -- 2.4.1 Relevant Stability -- 2.4.2 Performance Guaranteed Technique with Pre-defined Maximum Settling Time Function -- 2.4.3 Command Filter -- 2.4.4 Optimal Control Based on Adaptive Dynamic Programming -- 2.4.5 Differential Nonzero-Sum Games -- 2.4.6 Graph Theory -- 2.5 Brief Summary -- References -- Part I Performance Guaranteed Control for Single Spacecraft -- 3 Spacecraft Performance Guaranteed Asymptotic Control with Settling Time Constraints -- 3.1 Introduction -- 3.2 Spacecraft Attitude Performance Guaranteed Asymptotic Control -- 3.3 Simulation Analysis -- 3.4 Conclusion -- References -- 4 Spacecraft Finite-Time Performance Guaranteed Control -- 4.1 Introduction -- 4.2 Control Design and Stability Analysis Without Disturbances -- 4.3 Control Design and Stability Analysis with Disturbances -- 4.4 Simulation Analysis -- 4.4.1 Simulation Parameters.4.4.2 Performance and Comparison -- 4.5 Conclusion -- References -- 5 Spacecraft Performance Guaranteed Control with Improved Transient Performance -- 5.1 Introduction -- 5.2 Norm-Normalized Sign Function and Ratio Persistence -- 5.3 Control Design with Improved Transient Performance -- 5.3.1 Control Design and Stability Analysis Without Disturbances -- 5.3.2 Control Design and Stability Analysis with Disturbances -- 5.4 Simulation Analysis -- 5.4.1 Simulation Parameters -- 5.4.2 Performance and Comparison -- 5.5 Conclusion -- References -- 6 Spacecraft Performance Guaranteed Control with Command Filter -- 6.1 Introduction -- 6.2 Spacecraft Attitude Asymptotic Control Based on Command Filter -- 6.2.1 Control Design -- 6.2.2 Stability Analysis -- 6.3 Spacecraft Attitude Performance Guaranteed Asymptotic … -- 6.3.1 Control Design -- 6.3.2 Stability Analysis -- 6.4 Simulation Analysis -- 6.4.1 Simulation Parameters -- 6.4.2 Performance and Comparison -- 6.5 Conclusion -- References -- 7 Spacecraft Finite-Time Performance Guaranteed Control with Command Filter -- 7.1 Introduction -- 7.2 Control Design and Stability Analysis Without Disturbances -- 7.3 Control Design and Stability Analysis with Disturbances -- 7.4 Finite-Time Convergence Analysis of Command Filter Compensators -- 7.5 Simulation Analysis -- 7.5.1 Simulation Parameters -- 7.5.2 Performance and Comparison -- 7.6 Conclusion -- References -- 8 Spacecraft Performance Guaranteed Optimal Control with Adaptive Dynamic Programming -- 8.1 Introduction -- 8.2 Spacecraft Performance Guaranteed Optimal Control … -- 8.2.1 Control Design -- 8.2.2 Stability Analysis -- 8.3 Spacecraft Performance Guaranteed Optimal Control Based … -- 8.3.1 Control Design -- 8.3.2 Stability Analysis -- 8.4 Simulation Analysis -- 8.4.1 Simulation Parameters -- 8.4.2 Performance and Comparison -- 8.5 Conclusion -- References.Part II Performance Guaranteed Games for Multiple Spacecraft -- 9 Performance Guaranteed Non-Zero-Sum Games for Multiple Spacecraft -- 9.1 Introduction -- 9.2 Spacecraft Game Model and Preliminaries -- 9.2.1 Two-Spacecraft Attitude Game Model -- 9.2.2 Performance Guaranteed with Pre-defined Maximum Settling Time Function -- 9.2.3 Optimal Non-Zero-Sum Games and Nash Equilibrium -- 9.3 Performance Guaranteed NZS Game with Experience … -- 9.3.1 Algorithm Design -- 9.3.2 Stability Analysis -- 9.3.3 Nash Equilibrium Analysis -- 9.3.4 Multiple Spacecraft Situation -- 9.4 Simulation Analysis -- 9.4.1 Simulation Parameters -- 9.4.2 Performance and Comparison -- 9.5 Conclusion -- References -- 10 Performance Guaranteed Non-Zero-Sum Games for Combined Spacecraft -- 10.1 Introduction -- 10.2 Combined Spacecraft Game Model and Preliminaries -- 10.2.1 Combined Spacecraft Attitude Model with N Sets of Actuators -- 10.2.2 Performance Guaranteed Technique with Improved Performance Function -- 10.2.3 Optimal Non-Zero-Sum Games and Nash Equilibrium -- 10.3 Performance Guaranteed NZS Games with Experience Replay -- 10.3.1 Algorithm Design -- 10.3.2 Stability Analysis -- 10.3.3 Nash Equilibrium Solution -- 10.4 Simulation Analysis -- 10.4.1 Simulation Parameters -- 10.4.2 Performance and Comparison -- 10.5 Conclusion -- References -- Part III Performance Guaranteed Cooperation for Spacecraft Formation -- 11 Distributed Coordinated Control for Network Systems with Full-State Constraints -- 11.1 Introduction -- 11.2 Preliminaries and Problem Description -- 11.3 Control Design -- 11.3.1 Distributed Finite-Time Sliding-Mode Estimator -- 11.3.2 Distributed Coordinated Control with Full-State Constraints -- 11.4 Simulation -- 11.5 Conclusion -- References -- 12 Distributed Coordinated Control for Networked Spacecraft with Output Constraints -- 12.1 Introduction.12.2 Preliminaries and Problem Description -- 12.3 Control Design -- 12.3.1 Distributed Finite-Time Sliding-Mode Estimator -- 12.3.2 Full-State Feedback Control with Output Constraints -- 12.3.3 Output Feedback Control with Output Constraints -- 12.4 Simulation -- 12.5 Conclusion -- References -- 13 Formation-Containment Control for Networked Spacecraft with Output Feedback -- 13.1 Introduction -- 13.2 Preliminaries and Problem Description -- 13.3 First Layer: Distributed Formation Control Design for the Leaders -- 13.3.1 Distributed Finite-Time Sliding-Mode Estimator for Leaders -- 13.3.2 Distributed Formation Control of Leaders by Output Feedback -- 13.4 Second Layer: Distributed Containment Control Design for the Followers -- 13.4.1 Distributed Finite-Time Sliding-Mode Estimator for Followers -- 13.4.2 Distributed Containment Control of Followers by Output Feedback -- 13.5 Simulation -- 13.6 Conclusion -- References -- 14 Formation-Containment Control for Networked Spacecraft with Collision Avoidance -- 14.1 Introduction -- 14.2 Preliminaries and Problem Description -- 14.3 Distributed Formation-Containment Control with Collision … -- 14.4 Simulation -- 14.5 Conclusion -- References -- 15 Formation-Containment Control for Networked Spacecraft in Constrained Space -- 15.1 Introduction -- 15.2 Preliminaries and Problem Description -- 15.3 Layered Distributed Estimator -- 15.4 Layered Formation-Containment Control in Constrained Space -- 15.5 Simulation -- 15.6 Conclusion -- References -- 16 Conclusion.AstrodynamicsSpace vehiclesControl systemsSpace vehiclesPilotingAstrodynamics.Space vehiclesControl systems.Space vehiclesPiloting.629.4742Gao Yufeng1433310Li DongyuMiAaPQMiAaPQMiAaPQBOOK9910754087603321Spacecraft Maneuver with Performance Guaranteed3580374UNINA01784nam 2200385z- 450 9910346926103321202102121000010674(CKB)4920000000101261(oapen)https://directory.doabooks.org/handle/20.500.12854/61709(oapen)doab61709(EXLCZ)99492000000010126120202102d2009 |y 0gerurmn|---annantxtrdacontentcrdamediacrrdacarrierUntersuchungen zur Erzeugung von organischen Nanopartikeln mittels einer Flüssigkeitsring-VakuumpumpeKIT Scientific Publishing20091 online resource (XIX, 176 p. p.)3-86644-349-8 Die vorliegende Arbeit beschäftigt sich mit einer neuer Verfahrensidee zur aerosolbasierten Erzeugung von organischen Nanopartikeln. Durch simultane Kompression und Kühlung eines Gas-Dampf-Gemischs in einer Flüssigkeitsring-Vakuumpumpe tritt Aerosolbildung aufgrund homogener Keimbildung auf. Neben experimentellen Ergebnissen aus Versuchen an einer Pilotanlage liefert die Arbeit einen Modellansatz zur Beschreibung der schnelle Zustandsänderung und des Übersättigungsaufbaus in der Pumpe.Technology: general issuesbicsscAerosolFlüssigkeitsring-Vakuumpumpehomogene Keimbildungorganische NanopartikelnPartikelabscheidungTechnology: general issuesLauer Claudiaauth1304408BOOK9910346926103321Untersuchungen zur Erzeugung von organischen Nanopartikeln mittels einer Flüssigkeitsring-Vakuumpumpe3027373UNINA