摘要
分析了飞行仿真中飞机三自由度质点仿真模型机动指令生成器设计原理,并以蛇形机动飞行为例,建立了蛇形机动指令生成器数学模型。最后通过蛇形机动飞行仿真算例,验证了指令生成模型的合理性。结果表明,机动指令生成器能够完成仿真任务,从而将在飞机飞行仿真中得到广泛应用。
In this paper, we analyze the dynamic characteristics of the particle model of aircraft, which indicates that the changing of the flight states of aircraft is caused by the control variables. Based on the analysis, the principle of designing maneuver generator is proposed. Then the mathematical model of maneuver generator is built according to S maneuver command. The correct result of the simulation validates the mathematical model of the maneuver generator. The maneuver generator is able to accomplish aircraft flight simulation, so it will be widely used in the future.
出处
《飞行力学》
CSCD
北大核心
2005年第2期19-22,共4页
Flight Dynamics
