3Eggers A J, Allen J H. A comparative analysis of the performance of long-range hypervelocity vehicles[R]. NACA Technical Report, March 1954.
4Divya Garg, Michael A Patterson. Direct trajectory optimization and costate estimation of general optimal problems using a radan pseudospectral method[C]. AIAA Guidance, Navigation, and Control Conference. AIAA, August 2009.
5[苏]A.M.西纽科夫.固体弹道式导弹[M].北京:国防工业出版社,1984.
6DUKEMAN G A. Atmospheric ascent guidance for rocket- powered launch vehicles,AIAA2002- 4559[R]. 2002.
7DUKEMAN G A, CALISE A J. Enhancements to an atmospheric ascent guidance algorithm, AIAA2003 - 5638[R]. 2003.
8DUKEMAN G A. Closed-loop nominal and abort atmospheric ascent guidance for rocket-powered launch vehicles [ D]. Georgia : Georgia Institute of Technology, 2005.
9LU P,SUN H S,TSAI B. Closed-loop endoatmospheric ascent guidance[J]. Journal of Guidance, Control, and Dynamics, 2003,26(2):283- 294.
10LU P,ZHANG L J,SUN H S. Ascent guidance for responsive launch : a fixed-point approach, AIAA2005 - 6453[R]. 2005.
