Nonlinear Adaptive Flight Control Using Incremental Approximate Dynamic Programming and Output Feedback

被引：32
|
作者：
Zhou, Ye [1 ]
van Kampen, Erik-Jan [1 ]
Chu, QiPing [1 ]
机构：
[1] Delft Univ Technol, Aerosp Engn, Control & Simulat Div, NL-2629 HS Delft, Netherlands
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2017年 / 40卷 / 02期
关键词：
SYSTEMS; STRATEGIES; SPACECRAFT; INVERSION; DESIGN; MODEL;
D O I：
10.2514/1.G001762
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：493 / 500
页数：8
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