Method for controlling postures of aircraft converged at fixed time
An attitude control, fixed time technology, applied in the field of aircraft control
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[0093] In order to better illustrate the purpose and advantages of the present invention, the technical solution will be further described in detail below in conjunction with the accompanying drawings and examples.
[0094] Step 1: Establish a dynamic model of the re-entry vehicle, and propose a limited-time attitude tracking task.
[0095] Based on the attitude control problem of an unpowered reentry vehicle, the attitude dynamics equation is as follows:
[0096] ω · x = - I zz ( I zz - I yy ) + I xz 2 I * ...
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