[1] DI X GYANG Y F.Ascending trajectory optimization of near space airship based on genetic algorithm［C］//IEEE 8th Conference on Industrial Electronics and Applications (ICIEA)2013:918 922.

[2] DOU L QZONG QJI Y H.Robust dynamic inversion control for near space vehicle［C］//IEEE Proceedings of 3rd International Symposium on Systems and Control in Aeronautics and Astronautics2010:744 749.

[3] SHEN Q KJIANG BCOCQUEMPOT V.Fuzzy logic system based adaptive fault tolerant control for near space vehicle attitude dynamics with actuator faults［J］.IEEE Transactions on Fuzzy Systems201321(2):289 300.

[4] BUSCH MBLACKMAN S.Evaluation of IMM filtering foran air defence system application［C］//Proceedings of the SPIE Conference on Signal and Data Processing of Small Targets1995:435 447.

[5] BLACKMAN S SDEMPSTER R JROSZKOWSKI S H.IMM/MHT application to radar and IR multitarget tracking［C］//Proceedings of the SPIE Conference on Signal and Data Processing of Small Targets1997:429 439.

[9] HOULES ABAR SHALOM Y.Multisensor tracking of a maneuvering target in clutter［J］.IEEE Transactions on Aerospace and Electronic Systems198925(2):176 189.

[11] LI X RBAR SHALOM Y.Design of an interacting multiple model algorithm for air traffic control tracking ［J］.IEEE Transactions on Aerospace and Electronic Systems19931(3):186 194．

[12] BOLLINO K P.High fidelity real time trajectory optimization for reusable launch vehicles［D］.Monterey:Naval Postgraduate School2006.