Application of Unmanned Aircraft PID Control System for Roll, Pitch and Yaw Stability on Fixed Wings-Reference-Cited by-同舟云学术

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Application of Unmanned Aircraft PID Control System for Roll, Pitch and Yaw Stability on Fixed Wings

Published:2021-10-27 Issue: Volume: Page:
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Container-title:2021 International Conference on Computer Science, Information Technology, and Electrical Engineering (ICOMITEE)
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Author:

Susanto Try,Bayu Setiawan Muhammad,Jayadi Akhmad,Rossi Farli,Hamdhi Afrizal,Persada Sembiring Jaka

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9649654/9650077/09650314.pdf?arnumber=9650314

Cited by 10 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. Dual-loop control and state prediction analysis of QUAV trajectory tracking based on biological swarm intelligent optimization algorithm;Scientific Reports;2024-08-17

2. Autonomous Take-off Control System with Stall Prevention for Fixed-Wing UAVs Utilizing LQR Method;2024 IEEE 33rd International Symposium on Industrial Electronics (ISIE);2024-06-18

3. A Multi-Strategy Enhanced Marine Predator Algorithm for Global Optimization and UAV Swarm Path Planning;IEEE Access;2024

4. Q-Learning based system for Path Planning with Unmanned Aerial Vehicles swarms in obstacle environments;Expert Systems with Applications;2024-01

5. A Review of Reinforcement Learning for Fixed-Wing Aircraft Control Tasks;IEEE Access;2024

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