Key Technology Research on Stall Spin Simulation Training System of an Aircraft

doi:10.16182/j.issn1004731x.joss.22-0237

Abstract

Abstract:

Aiming at the domestic aircraft stall spin simulation training need, a stall spin simulation training system is developed. The training system consists of the multi-channel dome visual system, the semi-physical simulation cockpit and the maneuvering force control loading system, etc. Distributed simulation technology is used to develop a realistic man-in-the-loop simulation training environment. For the stall spin simulation, the multi-source aerodynamic data is processed comprehensively, and an unsteady aerodynamic model at high angle of attack (AOA) is constructed, and the heavy-load digital electric control loading technology is used to realize the simulation of stall spin alternating force and jitter characteristics of steering, which realizes the stall spin simulation training of man-in-the-loop.

Key words: stall spin, simulation and training, maneuvering force control loading, unsteady flow aerodynamics, man-in-the-loop

CLC Number:

TP391

Guangxu Xi, Yongyi Liu, Chong Wu, Junjie Zhang, Yinghao Chen. Key Technology Research on Stall Spin Simulation Training System of an Aircraft[J]. Journal of System Simulation, 2022, 34(4): 878-890.

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		资料1	资料2	资料3	资料4	资料5	资料6	资料7
升力系数
	基本升力系数	√	√	√	√	√	√	√
	升降舵产生的升力系数	√				√		√
	迎角变化率产生的升力系数
	地面效应产生的升力系数	√	√
	起落架产生的升力系数	√
	襟翼产生的升力系数	√	√
	发动机产生的升力系数
	外挂物产生的升力系数	√
	全机最大升力系数		√
	抖振升力系数		√		√

序号	部件名称	说明
1	左机翼	含左侧副翼和左侧襟翼
2	右机翼	含右侧副翼和右侧襟翼
3	左平尾	含左升降舵、左调整片
4	右平尾	含右升降舵、右调整片
5	机身	含起落架、减速板
6	垂尾	含方向舵、方向舵调整片

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