Flight speed and trajectory joint optimization method and system
A flight speed and joint optimization technology, which is applied in general control systems, control/regulation systems, non-electric variable control, etc., can solve problems such as inapplicable mass data transmission and poor system information throughput
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[0183] As an embodiment, the method of the present invention also includes:
[0184] Step S9: Calculate the minimum flight total energy consumption according to the optimal flight parameters, the specific formula is:
[0185]
[0186] Among them, E is the minimum total flight energy consumption, g is the acceleration of gravity, c 1 =ρC D0 S / 2 and c 2 = 2W 2 / [(πe 0 A R )ρS], ρ means air density, C D0 Indicates zero-lift drag coefficient, S indicates wing area, e 0 is the wingspan efficiency, W represents the overall weight of the UAV, and A R represents the aspect ratio of the drone's wing, and are the optimal flight radius, optimal flight speed, and optimal flight duration of the UAV in mode 1, respectively, and are the optimal flight speed and optimal flight time of UAV flying in mode 2, respectively, and are the optimal flight radius, optimal flight speed, and optimal flight duration of UAV flying in mode 3, respectively.
[0187]Step S1: Initialize,...
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