High Dynamic Staring Tracking Control Method for Non-coplanar Orbital Rendezvous Spacecraft Based on Fast Terminal Sliding Mode Controller

Author:

Geng Yunhai1,Sun Maojin1,Wu Fan1

Affiliation:

1. Harbin Institute of Technology,School of Astronautics,Harbin,China

Funder

National Natural Science Foundation of China

Publisher

IEEE

Reference25 articles.

1. Combined attitude control method of small satellite using reaction wheels and magnetorquers;chen;Journal of Jilin University(Engineering and Technology Edition),2010

2. Control allocation strategy for large angle maneuver and high precision stability control of agile small satellite;tang;Journal of Harbin Institute of Technology,2010

3. Research on fast maneuver and stabilization control algorithm for agile satellite;ye;Doctoral dissertation from Harbin Institute of Technology,2013

4. Spacecraft attitude control by combination of various torquers

5. Attitude tracking control for a space moving target with high dynamic performance using hybrid actuator

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