Incremental nonlinear dynamics inversion for attitude control of high-lift hybrid mode UAV transition process
Author:
Affiliation:
1. National University of Defense Technology,College of Aerospace Science and Engineering,Changsha,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10043103/10043201/10043218.pdf?arnumber=10043218
Reference8 articles.
1. Stability and Robustness Analysis and Improvements for Incremental Nonlinear Dynamic Inversion Control;ping;AIAA Guidance Navigation and Control Conference,2018
2. Comparison of Nonlinear Dynamic Inversion and Inverse Simulation
3. Transition between Level Flight and Hovering of a Tail-Sitter Vertical Takeoff and Landing Aerial Robot
4. Controller Design and Flight Test of the High-lift Hybrid Mode UAV
5. Small Unmanned Aircraft
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