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Attitude Takeover Control of Failed Spacecraft /

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Hlavní autoři: Huang, Panfeng (Autor), Zhang, Fan (Autor), Lu, Yingbo (Autor), Chang, Haitao (Autor), Zhang, Yizhai (Autor)
Médium: Elektronický zdroj E-kniha
Jazyk:angličtina
Vydáno: Amsterdam : Elsevier, 2024.
Témata:
Space vehicles > Control systems.
Véhicules spatiaux > Systèmes de commande.
Space vehicles > Control systems
On-line přístup:ScienceDirect
Tagy: Přidat tag
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Obsah:
  • Front Cover
  • Attitude Takeover Control of Failed Spacecraft
  • Copyright
  • Contents
  • List of figures
  • List of tables
  • Biographies
  • Panfeng Huang
  • Fan Zhang
  • Yingbo Lu
  • Haitao Chang
  • Yizhai Zhang
  • Preface
  • 1 Introduction
  • 1.1 Background of takeover control
  • 1.2 Manners of takeover control
  • 1.2.1 Rigid connection capturing
  • 1.2.2 Flexible connection capturing
  • 1.2.3 Cellular space robot capturing
  • 1.3 Research contents and chapter arrangement
  • References
  • 1 Space manipulator takeover control
  • 2 Trajectory prediction of space robot for capturing non-cooperative target
  • 2.1 Introduction
  • 2.2 Dynamic model
  • 2.3 EFIR/DFT filter design
  • 2.3.1 EFIR filter design
  • 2.3.2 DFT filter design
  • 2.4 Experiment realization and discussion
  • References
  • 3 Combined spacecraft stabilization control after multiple impacts during space robot capture of a tumbling target
  • 3.1 Introduction
  • 3.2 Attitude dynamics of the combined spacecraft and contact dynamics
  • 3.2.1 Problem description
  • 3.2.2 Attitude dynamics and kinematics
  • 3.2.3 Contact detection algorithm and contact dynamics model
  • 3.3 Stability control system design for combined spacecraft
  • 3.3.1 Conventional sliding mode controller design
  • 3.3.2 Improved sliding mode controller design
  • 3.3.3 Control redistribution based on pseudo-inverse
  • 3.4 Numerical simulations and experiments
  • References
  • 4 Attitude takeover control of a failed spacecraft without parameter uncertainties
  • 4.1 Introduction
  • 4.2 Attitude stability takeover control of target spacecraft based on reconstruction of a reaction wheel control system
  • 4.2.3.2 Control re-allocation based on dynamic control allocation method
  • 4.2.4 Numerical simulations
  • 4.3 Attitude coordinated control for docked spacecraft based on the estimated coupling torque of the space manipulator
  • 4.3.1 Attitude error dynamics of docked spacecraft
  • 4.3.1.1 Problem description
  • 4.3.1.2 Kinematics of space manipulator
  • 4.3.1.3 Attitude dynamics of a docked spacecraft
  • 4.3.1.4 Attitude error dynamics of a docked spacecraft
  • 4.3.2 Coordinated planning of a docked spacecraft attitude and a space manipulator
  • 4.3.2.1 Constraints
  • 4.3.2.2 Objective function

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