JEPPS G.Linearised optimal control and application to a gliding projectile[C]//AIAA Atmospheric Flight Mechanics Conference.Canberrn:AIAA,1985.
[2]
FLECK V.Increase of range for an artillery projectile by using the lifting force[C]//19th International Symposium on Ballistics.San Francisco:IBC,1996.
[3]
李瑜,杨志红,崔乃刚.助推-滑翔导弹弹道优化研究[J].宇航学报,2008,29(1):66-71. LI Yu,YANG Zhi-hong,CUI Nai-gang.A study of optimal trajectory for boost-glide missile[J].Journal of Astronautics,2008,29(1):66-67.(in Chinese)
[4]
CHEN Gang,HU Ying.Optimization design on RLV reentry trajectory based on genetic algorithm[J].Journal of Solid Rocket Technology,2006,29(4):235-238.
[5]
CHEN Gang,XU Min,WANG Zi-ming,et al.RLV reentry trajectory multi-objective optimization design based on NSGA-Ⅱ algorithm.AIAA-2005-6131[R].2005.
[6]
LOXTON R C,TEOA K L,REHBOCKA V.Optimal control problems with a continuous inequality constraint on the state and the control[J].Automatica,2009,45(10):2 250-2 257.
[7]
LOXTON R C,TEOA K L.Optimal control problems with multiple characteristic time points in the objective and constraints[J].Automatica,2008,44(11):2 923-2 929.
[8]
雷阳.一种求解最优控制问题的非均匀控制向量参数化方法[J].中国石油大学学报,2011,35(5):180-184. LEI Yang.A non-uniform control vector parameterization approach for optimal control problems[J].Journal of China University of Petroleum,2011,35(5):180-184.(in Chinese)
[9]
BRIAN C,FABIEN.Some tools for the direct solution of optimal control problems[J].Advances in Engineering Software,1998,29(1):45-61.
[10]
GOH C J,TEO L K.Control parameterization:a unified approach to optimal control problems with general constraints[J].Automatica,1988,24(1):3-18.
[11]
BETTS J T.Survey of numerical methods for trajectory optimization[J].Journal of Guidance,Control and Dynamics,1998,21(2):193-207.
[12]
MICHAEL R I,FARIBA F.A perspective on methods for trajectory optimization[C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit.Monterey,California:AIAA,2002.
