Rapid Optimal Generation Algorithm for Terrain Following Trajectory Based on Optimal Control

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.

作 者： 楊劍影 張海 謝邦榮 尹健   作者單位： 楊劍影,謝邦榮,尹健(School of Mechatronics Engineering, Beijing Institute of Technology,Beijing 100081, China)

張海(Department of Automatic Control, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) 

刊 名： 北京理工大學(xué)學(xué)報（英文版）  EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY  年，卷(期)： 2004 13(4)  分類號： V249.122  關(guān)鍵詞： terrain following(TF)   optimal control   objective function  

【Rapid Optimal Generation Algorithm f】相關(guān)文章：

第130講：dinks; sandwich generation05-04

《m f》教案02-23

學(xué)科術(shù)語 F05-04

維生素F01-28

航空縮略用語（F）05-04

《m f》教案設(shè)計08-26

天文術(shù)語 D-F05-04

《b p m f 》教學(xué)反思04-21

G-o-l-f(2)05-04

《b p m f》教案設(shè)計08-25