Distributed multi-rotor tilting wing aircraft control strategy analysis method
The invention relates to the field of flight mechanics and flight control of aircrafts, in particular to a distributed overdrive tilting wing aircraft control strategy analysis method. Comprising the following steps: step 1, determining a control surface distribution scheme; a control surface distri...
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| creator | SU BINGBING ZENG WEI CHEN LIXIA WANG ZHENGZHONG TIAN HONGYUAN LIU JIFU MA YUJIE HUANG SHUILIN HOU XIANGMIN CHEN JINHE |
| description | The invention relates to the field of flight mechanics and flight control of aircrafts, in particular to a distributed overdrive tilting wing aircraft control strategy analysis method. Comprising the following steps: step 1, determining a control surface distribution scheme; a control surface distribution scheme is determined based on a minimum control energy fusion method; the flight condition of the aircraft is not considered, control over the multiple pneumatic control surfaces is considered to be linked all the time, in order to give full play to the linkage efficiency of the multiple pneumatic control surfaces, the principle of weighted minimum control energy is adopted to distribute control input, and the control surfaces with high efficiency and large permission are used as much as possible under the same control input. Operation with low efficiency and small permission is not used as much as possible, and finally all control surface deflection angles are made to be as small as possible. 2, determining |
| format | Patent |
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Comprising the following steps: step 1, determining a control surface distribution scheme; a control surface distribution scheme is determined based on a minimum control energy fusion method; the flight condition of the aircraft is not considered, control over the multiple pneumatic control surfaces is considered to be linked all the time, in order to give full play to the linkage efficiency of the multiple pneumatic control surfaces, the principle of weighted minimum control energy is adopted to distribute control input, and the control surfaces with high efficiency and large permission are used as much as possible under the same control input. Operation with low efficiency and small permission is not used as much as possible, and finally all control surface deflection angles are made to be as small as possible. 2, determining</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING TRANSPORTING |
| title | Distributed multi-rotor tilting wing aircraft control strategy analysis method |
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