安全验证
第3期 章胜等:控制力矩陀螺辅助机动路径快速规划研究 67 Moment Gyroscopes[D].Austin,TX:Dept.of Computational and Applied Mathematics,Rice University,2007. [13]程迎坤,孙承启,张锦江.空间站力矩平衡姿态和动量平衡姿 态的研究[J 3.航天控制,2008,26(2):3-8. [14]Rao A V,Benson D,Darby C L.et a1.User’s manual for GPOPS version 5.O:A MATLAB software for solving muhiple—phase opti— mal control problems using hp adaptive pseudospeetral methods 1 10J Wie B,Barba P M.Quatemion feedback for spacecraft large angle maneuvers[J].Joumal of Guidance,1985,8(3):360~365. [11]Rao A V.A SurveY of Numerical Meth0ds for Ot)timal Control 【C].AAS/AIAA Astrodynamics Speciliast Conference.AAS Paper 09—334,Pittsburgh,PA,August 2009:1-32. [z].201I. 【15 J Gi11 P E,Murray W,Saunde ̄M A.User’S Guide for SNOPT 1 12 J Rao A V.A Primer on Pseudospeetral Methods for Solving Optimal Version 7:Software for Large-Scale Nonlinear Programming[Z], 20O6. Control Problems[z].Gainesville,FL,2011. Rapid path planning of Control Momentum Gyroscopes Assisting Maneuver ZHANG Sheng,HUANG Haibing,ZHAO Qian,TANG Guojin (College of Aerospace and Engineering,National University of Defense Technology,Changsha 410073,China) Abstract:As a new large angle maneuver technique concept for space station,Control Momentum Gyroscopes Assisting Maneuver (CMGs AM)is an efifcient technique which employs both the Control Moment Gyroscopes(CMGs)and thruster as the actuators.To enhance the performance of maneuver,the rapid planning of fuel-optimal CMGs AM path is studied.For the complex stu