Abstract Problems associated with determining the angular attitude of the unmanned aerial vehicle (UAV) with an inertial navigation system are considered. Some ways of its practical implementation using special test benches are proposed.
Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware
Russian Aeronautics ; 61 , 4 ; 605-612
2018-10-01
8 pages
Article (Journal)
Electronic Resource
English
Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware
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