ARTICLE
Analysis of an aircraft departure and spin characteristics using Nash equilibrium theory
1
School of Aircraft Engineering, Nanchang Hangkong University, China
Submission date: 2023-03-11
Final revision date: 2023-06-12
Acceptance date: 2023-06-16
Online publication date: 2023-09-15
Publication date: 2023-10-30
Corresponding author
Journal of Theoretical and Applied Mechanics 2023;61(4):647-658
KEYWORDS
TOPICS
ABSTRACT
The departure characteristics and steady-spin characteristics of a training aircraft are analyzed.
The sideslip departure characteristics of the aircraft under the maximum weight and
the minimum weight are obtained, respectively. When predicting the steady-spin, the equilibrium
point of the spin is found by an analytic-graphic method based on “Nash equilibrium
theory”, and the steady-spin parameters of this aircraft are obtained under the conditions
of maximum weight and minimum weight, left spin and right spin, neutral controls and prospin
controls. The simulation results have good theoretical significance for the optimization
and improvement of the aircraft in the preliminary design stage.
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| eISSN: | 2543-6309 |
| ISSN: | 1429-2955 |
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