Author:
Vachon Alexandre,Desbiens André,Gagnon Eric,Bérard Caroline
Reference33 articles.
1. A fast guidance algorithm for an autonomous navigation system;Teofilatto;Planet. Space Sci.,1998
2. Closed loop guidance of satellite launch vehicle – an overview;Shrivastava;J. Inst. Eng. (India),1986
3. G.A. Dukeman, Closed-loop nominal and abort atmospheric ascent guidance for rocket-powered launch vehicles (Ph.D. thesis), Georgia Institute of Technology, May 2005.
4. Optimal explicit guidance for three-dimensional launch trajectory;Sinha;Acta Astronaut.,1989
5. A. Mohammadi, J. Roshanian, M. Bahrami, B. Ebrahimi, On application of q-guidance method for satellite launch systems, in: Proceedings of the 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers, Harbin, China, 2010, pp. 1314–1319, http://dx.doi.org/10.1109/ISSCAA.2010.5632295.
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