A conventional layout helicopter and flight control method
A helicopter and layout technology, applied in the aviation field, can solve problems such as reducing aerodynamic efficiency, and achieve the effect of high forward flight speed and improved forward flight speed.
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[0045] The present embodiment provides a flight control method for a conventional layout helicopter 100, including the following steps:
[0046] S1. Obtain the current roll moment Mb and the maximum roll moment M of the short wing of the conventional layout helicopter 100 bmax , the minimum rolling moment M bmin and the current rolling moment M of the ABC single rotor 8 r ;
[0047] S2. Determine the current rolling moment M of the ABC single rotor 8 r The current roll moment M with the stub b , the maximum rolling moment M bmax , the minimum rolling moment M bmin size relationship;
[0048] S31. When the current rolling moment M of the ABC single rotor 8 r Greater than the maximum rolling moment M of the short wing bmax , obtain the rolling moment that the ABC single rotor 8 needs to reduce, expand the frame assembly 9 to the maximum and reduce the rolling moment of the ABC single rotor 8 to the target value. Specifically, the target value is the maximum rolling momen...
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