@inproceedings{00550acf75524b17a5143013466d6b23,
title = "Simulation and Control of Aircraft High Angle of Attack Stall Spin Based on Bifurcation Analysis Results",
abstract = "Stall spin is a hot topic in the field of flight dynamics in recent years. In order to solve the problem that conventional aerodynamic modeling and analysis are difficult to describe high angle of attack stall spin characteristics, the equilibrium point solution and stability analysis of the F-16 aircraft are carried out based on the bifurcation analysis method. With elevator deflection as a variable parameter, the global equilibrium solution of the aircraft and the relationship between its stability and elevator deflection are studied. A time domain simulation analysis of the aircraft model is carried out with an equilibrium state selected on the stall spin branch as the initial value, verifying the equilibrium and stability of the state. In addition, the entire stall spin entry to recovery is achieved by flight control. The simulation results show that the bifurcation analysis is very effective in studying the stall spin characteristics of aircraft at high angles of attack.",
keywords = "Bifurcation Analysis, Flight Control, Stall Spin",
author = "Zhouhang Wei and Jingping Shi and Yongxi Lyu and Shan Huang",
note = "Publisher Copyright: {\textcopyright} The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.; International Conference on Guidance, Navigation and Control, ICGNC 2024 ; Conference date: 09-08-2024 Through 11-08-2024",
year = "2025",
doi = "10.1007/978-981-96-2260-3\_14",
language = "英语",
isbn = "9789819622597",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "140--148",
editor = "Liang Yan and Haibin Duan and Yimin Deng",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 16",
}