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Adaptive Constrained On-board Guidance Technology for Powered Glide Vehicle

Huang Rong Wei Changzhu Liu Yanbin Lu Yuping

南京航空航天大学学报（英文版）2017，Vol.34Issue(2)：125-133,9.

Adaptive Constrained On-board Guidance Technology for Powered Glide Vehicle

Huang Rong ¹Wei Changzhu ²Liu Yanbin ¹Lu Yuping³

作者信息

1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, P.R.China
2. Beijing Institute of Control and Electronic Technology, Beijing 100038, P.R.China
3. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
折叠

摘要

关键词

adaptive constrained on-board guidance/double-pulse rocket engine/hp-adaptive Gauss pseudospectral method/powered quasi-equilibrium glide condition/linear quadratic regulator (LQR) trajectory tracking

Key words

分类

航空航天

引用本文复制引用

Huang Rong,Wei Changzhu,Liu Yanbin,Lu Yuping..Adaptive Constrained On-board Guidance Technology for Powered Glide Vehicle[J].南京航空航天大学学报（英文版）,2017,34(2):125-133,9.

基金项目

This work was supported by the National Natural Science Foundation of China (No.61403100) and Fundamental Research Funds for the Central Universities (HIT.NSRIF.2015037). （No.61403100）

南京航空航天大学学报（英文版）

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ISSN：1005-1120

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