Hypersonic flight vehicle angle-of-attack observation method based on nonlinear gain
A hypersonic, aircraft technology, used in the field of control
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[0051] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0052] The invention discloses a method for observing the angle of attack of hypersonic aircraft based on nonlinear gain. figure 1 As shown, the angle of attack observation system can be constructed by measuring the ballistic inclination angle and the attitude angle rate of the hypersonic vehicle, and a non- Linear variable gain error law, adjust the observed value of the angle of attack, estimate the force and moment of the aircraft through the observed value o...
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