Author:
Yamakawa Hiroshi,Funaki Ikkoh
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Reference22 articles.
1. CLOHESSY, W. H. and WILTSHIRE, R. S. “Terminal Guidance System for Satellite Rendezvous,” The Journal of the Astronautical Sciences, Vol. 27, No. 9, 1960, pp. 653–678.
2. ANTHONY, M. L. and SASAKI, F. T. “Rendezvous Problem for Nearly Circular Orbits,” AIAA Journal, Vol. 3, No. 9, 1965, pp. 1666–1673.
3. LONDON, H. S. “Second Approximation to the Solution of the Rendezvous Equations,” AIAA Journal, Vol. 1, No. 7, 1963, pp. 1691–1693.
4. CARTER, T. E. “New Form for the Optimal Rendezvous Equations near Keplerian Orbit,” Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1, 1990, pp. 183–186.
5. GIM, D.W. and ALFRIEND, K. T. “State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit,” Journal of Guidance, Control, and Dynamics, Vol. 26, No. 6, 2003, pp. 956–971.
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献