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轮控小型月球探测器姿态稳定的非线性预测控制 被引量:1

Nonlinear predictive control of the small lunar explorer three-axes attitude control using reaction wheels
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摘要 针对月球探测器飞行任务要求,推导三轴姿态稳定非线性预测控制器,以抑制反作用轮低速摩擦等对姿态的扰动,满足月球探测器高精度姿态稳定控制精度和稳定度的要求.仿真结果表明该控制器控制精度高,能有效抑制飞轮低速摩擦等对姿态的扰动. The small lunar explorer attitude control system, using reaction wheels as actuators, is a nonlinear system with coupling. In this paper, a nonlinear predictive three-axes attitude controller is developed to suppress reaction wheel low-speed friction effect and meet demand of lunar explorer attitude control system. Simulation results show that the controller proposed in this paper has excellent control precise and robustness, and can suppress reaction wheel low-speed friction effect effectively.
出处 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 2005年第4期507-511,共5页 Journal of Harbin Institute of Technology
关键词 非线性控制 预测控制 小型月球探测器 姿态控制 Computer simulation Control nonlinearities Friction Nonlinear control systems Predictive control systems Robustness (control systems) Vehicle wheels
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参考文献6

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同被引文献5

  • 1Ziegler B, Blanke M. Drag free motion control of satellite for high precision gravity field mapping [ C ]//Proceedings of the 2002 IEEE International Conference on Control Applications. 2002 : 292-297. 被引量:1
  • 2Prieto D, Bona B. A modem approach to drag attenuation in a H∞ robust orbit control[ C]//Proceedings of IEEE International Conference in Information and Communication Technologies. 2004 : 315-316. 被引量:1
  • 3Canuto E, Bona B,Indri M,et al. Drag free control for the European satellite GOCE ( Part I : modeling) [ C ]//Proceedings of the 41st IEEE Conference on Decision and Control Conference. 2002 : 1269-1274. 被引量:1
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  • 5曹喜滨,贺东雷.编队构形保持模型预测控制方法研究[J].宇航学报,2008,29(4):1276-1283. 被引量:8

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