Method for observing longitudinal motion state of aircraft by using time varying measurement delay output signal
A technology for longitudinal and delayed output of aircraft, which is applied in the field of flight control and can solve the problems of difficulty in designing observers and inconvenient design of control laws.
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[0058] The present invention will be further described in detail in conjunction with the accompanying drawings and implementation examples.
[0059] See Figure 7 , the present invention a kind of time-varying measurement delay output signal aircraft longitudinal movement state observation method, this method comprises the following steps:
[0060] Step 1: Obtain the dynamic model of the aircraft in the pitch plane
[0061] The observation object targeted by the present invention is an aircraft moving in a pitch plane. The schematic diagram of the structure of the aircraft in the pitch plane is as follows: figure 1 As shown, in this plane, the aircraft is subjected to the thrust from the engine, the lift and drag force exerted by the air, and the pitching moment. By analyzing the force received, the dynamic equation of the aircraft in the longitudinal motion can be obtained. After linearizing it, the dynamic model expression as shown below can be obtained:
[0062] ...
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