Switched Model-Predictive-Control-Based Trajectory Tracking of Fixed-Wing Aircraft for Payload Dropping

被引：2

作者：

Li, Yunpeng ^{[1
]}

Zhang, Lixian ^{[1
]}

Wu, Tong ^{[1
]}

Han, Yuejiang ^{[1
]}

Zhang, Yuxuan ^{[1
]}

机构：

[1] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Peoples R China

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2025年 / 48卷 / 03期

基金：

中国国家自然科学基金;

关键词：

Fixed Wing Aircraft; Model Predictive Control; Aircraft Flight Control System; Feedback Control; Flight Path Angle; Aircraft Stability and Control; Payload Dropping; Switched Control; Trajectory Tracking; SYSTEMS; DESIGN;

D O I：

10.2514/1.G008074

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：679 / 688

页数：10

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