Sideslip angle estimation based active disturbance rejection 3D trajectory tracking control for powered parafoil system and hardware-in-the-loop simulation verification
Author:
Funder
National Natural Science Foundation of China
Key Technologies Research and Development Program
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference43 articles.
1. Autonomous homing control of a powered parafoil with low altitude;Tao;ISA Trans.,2016
2. Wind-field identification for parafoils based on deep Q-learning iterative inversion;Yu;Inf. Sci.,2022
3. Research on the aerodynamic performance of parafoil for autonomous recovery;Li,2021
4. Accurate flight path tracking control for powered parafoil aerial vehicle using ADRC-based wind feedforward compensation;Luo;Aerosp. Sci. Technol.,2019
5. Distributed consensus algorithm for multiple parafoils in mass airdrop mission based on disturbance rejection;Sun;Aerosp. Sci. Technol.,2021
Cited by 2 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. Compensation control strategy for photoelectric stabilized platform based on disturbance observation;Aerospace Science and Technology;2024-02
2. Intelligent Trajectory Tracking Linear Active Disturbance Rejection Control of a Powered Parafoil Based on Twin Delayed Deep Deterministic Policy Gradient Algorithm Optimization;Applied Sciences;2023-11-21
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