Frequency‐Domain Idenitification of XV‐15 Tilt‐Rotor Aircrart Dynamics in Hovering Flight
Author:
Affiliation:
1. Aeromechanics Laboratory, U.S. Army Research and Technology Laboratories—AVSCOM, Moffett Field, CA
Publisher
American Helicopter Society
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. Modeling and Dynamic Analysis of a Distributed Propulsion Tilt-Rotor Aircraft;AIAA AVIATION 2022 Forum;2022-06-20
2. A novel system identification algorithm for quad tilt-rotor based on neural network with foraging strategy;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-12-08
3. References;Helicopter Flight Dynamics;2018-09-08
4. Aerodynamic Derivative Calculation Using Radial Basis Function Neural Networks;Advanced UAV Aerodynamics, Flight Stability and Control;2017-05-05
5. Flight Testing, Data Collection, and System Identification of a Multicopter UAV;AIAA Modeling and Simulation Technologies Conference;2017-01-05
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