The trajectory planning of spacecraft based on optimal quintic polynomial

Yanghua Li, Bo Mo

科研成果: 会议稿件论文同行评审

3 引用 (Scopus)

摘要

This paper focuses on the implementation and application of the quintic polynomial in the spacecraft trajectory planning. Firstly, the kinematics model and dynamics model of the spacecraft is established. Secondly, the PID control algorithm is used to control the spacecraft. Thirdly, in order to achieve fast and flexible of the spacecraft attitude maneuver, the coefficients of the quintic polynomial are adjusted continuously to optimize the spacecraft. At last, this paper uses Simulink for the simulation, such that the maneuver which is not less than 40 ° is completed within a predetermined period of time angle and such that the attitude angle, attitude angular velocity, and posture angular acceleration can be smoothed.

源语言英语
865-868
页数4
DOI
出版状态已出版 - 2013
活动2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013 - Harbin, 中国
期限: 16 8月 201318 8月 2013

会议

会议2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013
国家/地区中国
Harbin
时期16/08/1318/08/13

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引用此

Li, Y., & Mo, B. (2013). The trajectory planning of spacecraft based on optimal quintic polynomial. 865-868. 论文发表于 2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013, Harbin, 中国. https://doi.org/10.1109/MIC.2013.6758098