Author:
Chawla C.,Sarmah P.,Padhi R.
Reference31 articles.
1. A proposed international tropical reference atmosphere upto 1000 km;Ananthasayanam;Advances in Space Research,1987
2. R. Arora, M.R. Ananthasayanam, Trajectory design for a reusable launch vehicle demonstrator during re-entry phase, in: Proceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit, AIAA-2003-5547, 2003.
3. An Introduction to Numerical Analysis;Atkinson,2001
4. Practical Method for Optimal Control Using Nonlinear Programming;Betts,2001
5. K.P. Bollino, I.M. Ross, D.D. Doman, Optimal nonlinear feedback guidance for reentry vehicles, in: Proceedings of AIAA Guidance Navigation and Control Conference and Exhibit, AIAA-2006-6074, 2006.
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