Influence of flight control law on spin dynamics of aerodynamically asymmetric aircraft
Author:
Publisher
Polish Society of Theoretical and Applied Mechanics
Subject
Mechanical Engineering
Cited by 6 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. Optimization of steady spin prediction by nonlinear iterative inversion algorithm;Aircraft Engineering and Aerospace Technology;2024-06-20
2. Analysis of an aircraft departure and spin characteristics using Nash equilibrium theory;Journal of Theoretical and Applied Mechanics;2023-09-15
3. Objective comparison of numerical spin study with aircraft model free-flight spin tests;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-05-23
4. On the modeling of asymmetric disturbance effect and rejection control for fixed-wing aircraft;International Journal of Modeling, Simulation, and Scientific Computing;2022-03-12
5. A review and historical development of analytical techniques to predict aircraft spin and recovery characteristics;Aircraft Engineering and Aerospace Technology;2020-07-13
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