Design of a Smooth Landing Trajectory Tracking System for a Fixed-wing Aircraft
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/8789884/8814292/08814912.pdf?arnumber=8814912
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A Novel Integrated Flight Simulation Framework: From Actuators to High-Fidelity Dynamics to Flight Visualization;2024 Integrated Communications, Navigation and Surveillance Conference (ICNS);2024-04-23
2. Design of Optimal Iterative Learning Control Autopilot for Landing Fixed-Wing Aircraft;2023 31st International Conference on Electrical Engineering (ICEE);2023-05-09
3. Automatic Landing System Design and Simulation of a Fixed-Wing UAV;AIAA AVIATION 2022 Forum;2022-06-20
4. Backstepping and dynamic inversion control techniques for automatic landing of fixed wing unmanned aerial vehicles;Aerospace Science and Technology;2022-01
5. A Landing Trajectory Tracking Controller for Fixed-Wing UAV Based on Iterative Learning Control;Lecture Notes in Electrical Engineering;2021-11-02
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