A Direct Parametric Approach to Spacecraft Attitude Tracking Control

Xiao-Yi Wang and Guang-Ren Duan. A Direct Parametric Approach to Spacecraft Attitude Tracking Control. International Journal of Automation and Computing, vol. 14, no. 5, pp. 626-636, 2017 doi:  10.1007/s11633-017-1089-4
 Citation: Xiao-Yi Wang and Guang-Ren Duan. A Direct Parametric Approach to Spacecraft Attitude Tracking Control. International Journal of Automation and Computing, vol. 14, no. 5, pp. 626-636, 2017
##### doi: 10.1007/s11633-017-1089-4

National Natural Science Foundation of China 61321062

## A Direct Parametric Approach to Spacecraft Attitude Tracking Control

Funds:

National Natural Science Foundation of China 61321062

###### Corresponding author:Xiao-Yi Wang received the B. Sc. degree from Department of Control Science and Engineering, Harbin Institute of Technology, China in 2014. She received the M. Sc. degree in Centre for Control Theory and Guidance Technology, Harbin Institute of technology, China in 2017.     Her research interests include nonlinear robust control and spacecraft attitude control.     E-mail:xiaoyiwang51@outlook.com (Corresponding author)     ORCID iD:0000-0002-8511-1273
• Figure  1.  Error attitude quaternion ${q} _e$

Figure  2.  Response curve of variable ${e}$ and $\dot{e}$ of controlled system

Figure  3.  Comparison between controlled spacecraft attitude and target spacecraft attitude

Figure  4.  Controller ${u}$ with respect to time curve

Figure  5.  Response curve of variable ${e}$ and $\dot{e}$ of controlled system

Figure  6.  Curve of the state error between practical system and theoretical system

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##### 出版历程
• 收稿日期:  2016-08-19
• 录用日期:  2017-03-29
• 网络出版日期:  2017-07-03
• 刊出日期:  2017-10-01

## A Direct Parametric Approach to Spacecraft Attitude Tracking Control

##### doi: 10.1007/s11633-017-1089-4
基金项目:

National Natural Science Foundation of China 61321062

### English Abstract

Xiao-Yi Wang and Guang-Ren Duan. A Direct Parametric Approach to Spacecraft Attitude Tracking Control. International Journal of Automation and Computing, vol. 14, no. 5, pp. 626-636, 2017 doi:  10.1007/s11633-017-1089-4
 Citation: Xiao-Yi Wang and Guang-Ren Duan. A Direct Parametric Approach to Spacecraft Attitude Tracking Control. International Journal of Automation and Computing, vol. 14, no. 5, pp. 626-636, 2017

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