Adaptive Sliding Mode Control for Spacecraft Autonomous Rendezvous With Elliptical Orbits and Thruster Faults

Adaptive Sliding Mode Control for Spacecraft Autonomous Rendezvous With Elliptical Orbits and Thruster Faults

This paper investigates the problem of spacecraft autonomous rendezvous control for elliptical target orbits with external disturbance and thruster faults. The Clohessy-Wiltshire equation of elliptical target orbits without linearization is employed to describe the relative dynamic model as a linear...

Full description

Bibliographic Details
Main Authors: Ruixia Liu, Zhaowei Sun, Dong Ye
Format: Article
Language:English
Published: IEEE 2017-01-01
Series:IEEE Access
Subjects:
Spacecraft rendezvous
adaptive control
sliding mode control
thruster faults
Online Access:https://ieeexplore.ieee.org/document/8086152/

Internet

https://ieeexplore.ieee.org/document/8086152/

Similar Items