Simple Guidance Scheme for Low-Thrust Orbit Transfers

Simple Guidance Scheme for Low-Thrust Orbit Transfers
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DOI:
10.2514/2.4344
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发表时间:
1998-11
影响因子:
2.6
通讯作者:
C. Kluever
C. Kluever
中科院分区:
工程技术3区
文献类型:
--
作者:
C. Kluever

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3PAO,L.Y.,<柔性结构的最短时间控制特性>,《制导、控制和动力学杂志》,第19卷,第1期,1996年,第123-129页。4 Singh,T.和Vadali,S.R.,“RobustTime-Optimal Control:AFfurency域方法”,“制导、控制和动力学杂志”,第17卷,第2期,1994年,第346-353页。5Singer,N.C.,and Seering,W.P.,“Preshaping Command Installation to Reduced System Vivisis”,《动力系统、测量与控制杂志》,第12卷,1990年3月,第76-82页。6 Banerjee,A.K.,“航天飞机-天线系统的动力学和控制”,“宇航科学杂志”,第41卷,1993年1-3月,第73-90页。7 Singhose,W.,Banerjee,A.K.,和Seering,W.E.,“SleingingFlexticalServailers with Decections Limit Inpution Shape”,《制导、控制和动力学杂志》,第20卷,第2期,1997年,第291-298页。8 Singhose,W.和Singer,N.,<输入成形对二维轨迹的影响>,《IEEE机器人和自动化学报》,第12卷,第6期,1996年,第881-887页。9 Spong,M.W.和Vidyasagar,M.,RobotDynamics and Control,Wiley,New York,1989,pp.24,259-283。10Banerjee,A.K.和Singhose,W.E.,《两连杆柔性机器人的非线性跟踪控制的输入整形》,AAS/AIAA天体动力学专家会议,AAS论文97-121,太阳谷,ID,1997年8月。
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