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美军OODA循环周期缩短原因浅析 被引量:4

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出处 《国防科技》 2005年第7期65-67,共3页 National Defense Technology
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  • 1付东,方程,王震雷.作战能力与作战效能评估方法研究[J].军事运筹与系统工程,2006,20(4):35-39. 被引量:67
  • 2Palfalvy G M, Andes D K. Technology related to the highly maneuverable lethal vehicle ( HMLV ) concept [ R ]. AGARD - CP594, 1998.
  • 3Wunderlich G, langler W. Preliminary considerations concerning a high-g UCAV design[ A]. UAVS 15th International Conference 10-12[C], Bristol, United Kingdom, 2000, 1-6.
  • 4Flach J M, Eggleston R G, Kuperman G G, et al. SEAD and the UCAV: a preliminary cognitive systems analysis it [ R ].AFRL - HE - WP - TR - 1998 -0013, 1998.
  • 5[EB] http: //www. darpa, mil/j - ucas/.
  • 6Bookstaber D. Unmannod Combat Aerial Vehicles - What men do in aircraft and why machines can do it better[ EB] . http: www. airpower Maxwell af. mil/airchronides/ec/ucav, pdf.
  • 7总装备部电子信息基础部.现代武器装备知识书-导弹武器与航天器装备[M].北京:原子能出版社,航空工业出版社,兵器工业出版社,2003.
  • 8Lee D S, Gonzalez L F, Srinivas K, et al. Aerodynamic/RCS shape optimisation of unmanned aerial vehicles using hierarchical asynchronous parallel evolutionary algorithms [ R ]. AIAA 2006 -3331, 2006.
  • 9Enns D. Control allocation approaches[ R]. AIAA 98 - 4109, 1998.
  • 10Buffington J M. Modular control law design for the Innovative Control Effcctors( ICE )tailless fighter aircraft configuration 101 -3[R]. AFRL-VA-WP-TR-1999-3057, 1999.

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