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Satellite-Ground Link Planning Method for LEO Satellite Navigation Augmentation Network in the Case of Multiple Ground Stations Read chapter Read first chapter

2022 | OriginalPaper | Chapter

Aircraft Trajectory Tracking Method Based on Terminal Angle Constraint and Inverse Proportional Guidance Obstacle Avoidance

Authors : Linxu Wu, Fengjuan Guo, Jiayu Liu, Jiale Han

Published in: China Satellite Navigation Conference (CSNC 2022) Proceedings

Publisher: Springer Nature Singapore

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Abstract

Aiming at the issue of autonomous path tracking and obstacle avoidance of aircraft, in order to suppress the significant change of the speed direction during the path tracking process, the terminal angle constraint item is introduced into the guidance law to realize the smooth tracking of each path point. In addition, based on the relative positional relationship and movement direction between the aircraft and the obstacle, the obstacle avoidance guidance law is established in the target line of sight coordinate system in this paper. At the same time, the speed control item in the process of avoiding obstacles has been added. Through simulation, the aircraft which manipulated by the guidance law can achieve smooth tracking of the preset path and effectively avoid unexpected obstacles in the path as well.

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previous chapter Design and Implementation of Intelligent Operation and Maintenance of BDS-3 RNSS Service
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Metadata
Title
Aircraft Trajectory Tracking Method Based on Terminal Angle Constraint and Inverse Proportional Guidance Obstacle Avoidance
Authors
Linxu Wu
Fengjuan Guo
Jiayu Liu
Jiale Han
Copyright Year
2022
Publisher
Springer Nature Singapore
Book
China Satellite Navigation Conference (CSNC 2022) Proceedings

Print ISBN: 978-981-19-2579-5

Electronic ISBN: 978-981-19-2580-1

Copyright Year: 2022

DOI
https://doi.org/10.1007/978-981-19-2580-1_24