Method for distinguishing aircraft motion mode
一种运动模态辨识、运动模态的技术,应用在模拟器、仪器、自适应控制等方向,能够解决飞机系统数学模型复杂、很难飞机性能做出正确的评价等问题
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[0066] Given the flight test data of a certain type of aircraft (H=3km, M=0.3, T=0.05), the algorithm introduced in this paper is used to solve the identification parameters.
[0067] The aircraft longitudinal short-period motion mode usually uses the following equivalent mathematical model:
[0068]
[0069] In the formula is the pitch rate (rad / s), F p is the longitudinal bar force (lb), is the equivalent gain (rad / sec / lb), is the short-period mode equivalent natural frequency (rad / sec), is the reciprocal of the short-period mode equivalent time constant (1 / sec), and τ is the equivalent time delay (sec).
[0070] Here, the first-order Bode approximation is used,
[0071]
[0072] The above formula is transformed into a continuous linear differential equation through pull-type inverse transformation:
[0073] d 3 θ · ( ...
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