Robust Motion Planning for a Differentially Flat Fixed-Wing Aircraft

被引:0
|
作者
Aldabbas, Samer Raed [1 ,2 ]
Abu-Khalaf, Murad [2 ]
Koyuncu, Emre [1 ]
机构
[1] Istanbul Tech Univ, Aerosp Res Ctr, Istanbul, Turkiye
[2] Turkish Aerosp, Air Vehicle Technol Res Ctr, Istanbul, Turkiye
来源
IFAC PAPERSONLINE | 2024年 / 58卷 / 30期
关键词
trajectory planning; aircraft control; coordinated flight; dynamic feedback linearization; wind frame;
D O I
10.1016/j.ifacol.2025.01.180
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper investigates robustness and sensitivity in autonomous flight trajectory planning, focusing on model uncertainties during frame transitions. We analyze the role of differential flatness in planning open-loop state-control trajectories and examine how uncertainties impact robustness when mapped from the wind frame to the body frame. Using the given coordinated flight model, we assess mapping errors under mass uncertainty, reflecting these uncertainties back to the wind frame for analysis. Numerical simulations of a barrel roll maneuver illustrate our findings, contributing to the development of resilient trajectory planning frameworks for autonomous flight under variable conditions. Copyright (c) 2024 The Authors.
引用
收藏
页码:197 / 202
页数:6
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