Research on Control Method of Deployable Thrust Pointing Mechanism for Electric Propulsion

Author:

Lv Zhenhua1,Wen Wen1,Liu Lumi1,Zhang Meng1,Liu Weihui1,Wu Shujie1

Affiliation:

1. Beijing Institute of Control Engineering,Beijing,China

Publisher

IEEE

Reference11 articles.

1. A High-precision Acceleration and Deceleration Control of 7-segment Dissymmetrical S-shape Curve for Look-ahead;haihong;Mechanical Science and Technology for Aerospace Engineering,2016

2. Research status and prospect of chemical-electrospray dual-mode propulsion system[J];qinqin;Chinese Space Science and Technology,2021

3. Research on S Type Acceleration and Deceleration Time Planning Algorithm with Beginning and End Speed Non-zero[J];liangliang;Journal of Mechanical Engineering,2016

4. Design of Next-Generation All-Electric Telecommunication Satellites

5. Finding a Way: Boeing's All Electric Propulsion Satellite

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