Reentry flight attack angle guiding method of sub-orbital vehicle
An aircraft and sub-orbital technology, applied in the field of guidance and control, can solve problems such as large normal overload peaks
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[0069] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0070] In view of this, the object of the present invention is to provide an angle of attack guidance method for suborbital vehicle re-entry flight, which can reduce the normal overload peak value during the re-entry process of the vehicle.
[0071] During the reentry flight of a suborbital vehicle, its aerodynamic force can be approximately expressed as:
[0072] F = L 2 + D 2 L = 1 ...
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