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Rapid Optimal Generation Algorithm for Terrain Following Trajectory Based on Optimal Control 被引量:1

Rapid Optimal Generation Algorithm for Terrain Following Trajectory Based on Optimal Control
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摘要 Based on the optimal control theory, a 3-dimensionnal direct generation algorithm is proposed for anti-ground low altitude penetration tasks under complex terrain. By optimizing the terrain following(TF) objective function,terrain coordinate system, missile dynamic model and control vector, the TF issue is turning into the improved optimal control problem whose mathmatical model is simple and need not solve the second order terrain derivative. Simulation results prove that this method is reasonable and feasible. The TF precision is in the scope from 0.3 m to 3.0 m,and the planning time is less than 30 min. This method have the strongpionts such as rapidness, precision and has great application value. Based on the optimal control theory, a 3-dimensionnal direct generation algorithm is proposed for anti-ground low altitude penetration tasks under complex terrain. By optimizing the terrain following(TF) objective function,terrain coordinate system, missile dynamic model and control vector, the TF issue is turning into the improved optimal control problem whose mathmatical model is simple and need not solve the second order terrain derivative. Simulation results prove that this method is reasonable and feasible. The TF precision is in the scope from 0.3 m to 3.0 m,and the planning time is less than 30 min. This method have the strongpionts such as rapidness, precision and has great application value.
出处 《Journal of Beijing Institute of Technology》 EI CAS 2004年第4期406-409,共4页 北京理工大学学报(英文版)
关键词 terrain following(TF) optimal control objective function terrain following(TF) optimal control objective function
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  • 1NAVALPostgraduateSchool.Conceptualdesignofastand offeaponformaritimepatrolaircraft[R ][]..1989
  • 2HuShousong.Theprincipleofautomaticcontrol[M ][]..1994
  • 3SwansonRS,MusaS.Theestimationofobstacleandterrainclobberprobabilities. AIAA 75-1118 . 1975
  • 4Griswold M R.AFTI/F-16 automated maneuvering attack system AMAS guidance and control[].Proceedings of the IEEE National Aerospace and Electronics Conference.1986
  • 5Gordon F W.Automated maneuvering attack system safety design[].Proceedings of the IEEE National Aerospace and Electronics Conference.1986
  • 6Wilber G F.Automated strategic relocatable target mission planning[].Proceedings of the IEEE National Aerospace and Electronics Conference.1989
  • 7Asseo J.Terrain following/terrain avoidance path optimization using the method of steepest descent[].Proceedings of the IEEE National Aerospace and Electronics Conference.1982
  • 8Lu Ping.Optimal control problems with maximum functional[].Journal of Guidence Control and Dynamics.1991
  • 9Mennon P,Kim E.Optimal trajectory synthesis for terrain following flight[].Journal of Guidence Control and Dynamics.1991

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