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APPLICATION OF VELOCITY GAIN GUIDANCE TO FAR-DISTANCE RENDEZVOUS
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作者 刘鲁华 汤国建 +1 位作者 郑伟 余梦伦 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2006年第3期168-172,共5页
Using impulse hypothesis to solve far-distance rendezvous is difficult to be realized in a real project and the guidance accuracy cannot be controlled. A two-maneuver guidance law is designed for the two-impulse rende... Using impulse hypothesis to solve far-distance rendezvous is difficult to be realized in a real project and the guidance accuracy cannot be controlled. A two-maneuver guidance law is designed for the two-impulse rendezvous problem. The velocity gain guidance is applied to the first maneuver and the time-cut-off law is applied to the second one. Theoretical and simulation results show that the plan is credible. Accuracy requirements in fardistance rendezvous and in transform to close-in rendezous can be met. 展开更多
关键词 velocity gain guidance RENDEZVOUS guidance accuracy C-W equation
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