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助推-滑翔飞行器弹道分段优化研究

李柯 聂万胜 冯必鸣

指挥控制与仿真2012,Vol.34Issue(5):21-25,5.
指挥控制与仿真2012,Vol.34Issue(5):21-25,5.DOI:10.3969/j.issn.1673-3819.2012.05.006

助推-滑翔飞行器弹道分段优化研究

Research on Multi-Phase Trajectory Optimization for Boost-Glide Vehicle

李柯 1聂万胜 1冯必鸣1

作者信息

  • 1. 装备学院,北京101416
  • 折叠

摘要

Abstract

The dynamics parameters of the lifting body were calculated by numerical simulation . The boost-glide vehicle's trajectory was divided into two phases: power flight phase and glide phase .By Radau pseudospectral method, the trajectory optimization planning problem was converted into nonlinear planning problem. A integral trajectory from launch to glide was obtained by software simulating. The effect of the performance index of power flight on the maximum range was analyzed. The results show that the optimization project of which performance index was maximum speed had longer range and moderate difficulty.

关键词

伪谱法/助推滑翔/弹道优化/最大射程/分段

Key words

pseudospectral/ boost-glide/ trajectory optimization/ maximun range/ multi-phase

分类

航空航天

引用本文复制引用

李柯,聂万胜,冯必鸣..助推-滑翔飞行器弹道分段优化研究[J].指挥控制与仿真,2012,34(5):21-25,5.

指挥控制与仿真

OACSTPCD

1673-3819

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