Spacecraft Electromagnetic Docking and Separation

Häftad, Engelska, 2026

1 584 kr

Kommande

Beskrivning

Spacecraft Electromagnetic Docking and Separation in Elliptical Orbits solves problems for spacecraft electromagnetic docking and separation control system using different control methods: instead of the widely used proportional-integral-derivative controller or PID control. The book focuses on presenting a variety of control strategies tailored for spacecraft electromagnetic docking and separation, accompanied by stability proofs that integrate Lyapunov stability theory with sliding mode theory, LMIs-based theorems, model predictive control theories, reinforcement study theories and other frameworks, so the reader can understand how to handle different kinds of disturbances and perturbations in actual orbiting spacecraft. The book also provides a review of magnetic field, magnetic field force model (both the near-field model and the far-field model), useful lemmas and dynamic modelling methods of spacecraft relative motion, which can serve as first stage analysis for further research and are especially important in the initial design phase of a spacecraft electromagnetic docking and separation control system

A wide variety of novel robust and non-fragile controllers are discussed and against a backdrop of considering various uncertainties, e.g. advanced sliding mode control, observer-based control, model predictive control, reinforcement study-based control and impedance control; these are not only applicable to spacecraft electromagnetic docking and separation control, but also easily extendable to a more general class of second-order system with uncertainties and perturbations
Discusses the mathematical representation of spacecraft electromagnetic docking and separation control systems with uncertainties embedded in them leads to a model-like continuous and discrete state-space form which makes the developed controller universal
Discusses the role, in spacecraft electromagnetic docking and separation, of how the control systems in achieving high-precision position and better robustness to external disturbances (plus various uncertainties and gain perturbations) can be achieved

Produktinformation

Utgivningsdatum:2026-09-01
Mått:152 x 229 x undefined mm
Vikt:450 g
Format:Häftad
Språk:Engelska
Antal sidor:400
Förlag:Elsevier Science
ISBN:9780443493348

Utforska kategorier

Mer om författaren

Keke Shi is an Associate Professor at Xi’an University of Science and Technology, China. Dr Shi’s research interests include spacecraft electromagnetic docking and separationChuang Liu is an Associate Professor at Northwestern Polytechnical University, China. He is also Scientific Committee Member of Aeromeet 2022. He received the COSPAR Outstanding Paper Award for Young Scientists in 2020. His research focuses on aerospace engineering. Xiaokui Yue is a Professor at Northwestern Technical University, China. His research has focused on the frontiers of space exploration and on computational methods for nonlinear dynamical systems. Mahe Shu is a PhD research student at Northwestern Polytechnical University. Research interests include spacecraft electromagnetic docking and separation

Innehållsförteckning

1. Introduction of basic knowledge2. Coupled Orbit-Attitude Tracking Control for Spacecraft Electromagnetic Docking3. Intermediate Observer-based Control for Spacecraft Electromagnetic Docking4. Active Disturbance Rejection Control for Spacecraft Electromagnetic Docking5. Disturbance Observer-based Control for Spacecraft Electromagnetic Docking6. Model Predictive Control for Spacecraft Electromagnetic Docking7. Deep Reinforcement Learning-based Control for Spacecraft Electromagnetic Docking8. Sliding Mode Tracking Control for Spacecraft Electromagnetic Separation9. Optimizations-based Impedance Control for Spacecraft Electromagnetic Separation10. Integrated Control for Spacecraft Electromagnetic Docking and Separation