A new control method for rotary-wing drones
A technology of unmanned rotor control method, applied in attitude control, control/regulation system, non-electric variable control and other directions, can solve the problems of complex algorithm, complex calculation, narrow practical situation, etc., and achieve good robustness and control accuracy. high effect
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[0188] In this example, it is assumed that the mass m=1.373kg
[0189] J x =0.10125kg m 2 ,J y =0.10203kg·m 2 ,J z =0.14374kg·m 2
[0190] J xy =0.00217kg·m 2 ,J yz =0.00153kg·m 2 ,J zx =0.00030kg·m 2
[0191] Available parameters are:
[0192] Table 1 Parameter calculation table (kg m 2 )
[0193]
[0194]
[0195] According to (18) and Theorem 1, determine the parameter z that makes the state equation of the S system stable 1 ,z 2 .
[0196] Thanks to J z It is the largest among the various elements of the moment of inertia, so when determining z 1 ,z 2 when, -W 33 The strictly diagonally dominant condition will be decisive.
[0197] Let the maximum value of angular velocity in three directions be 10rad / s.
[0198] remember
[0199]
[0200]
[0201]
[0202] The condition of equation (22) is satisfied to ensure the stability of the state equation of the S system.
[0203]
[0204]
[0205] Estimate z by formula (22), (23) 1 ,z ...
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