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Abstract:
To achieve a desired formation of multiple unmanned aerial vehicles (UAVs), especially small and identical fixed-wing UAVs with limited computational capability, a practical leader-follower formation control method based on nonlinear control with positive velocity and saturated heading rate constraints is proposed in this paper, in which a heading angle controller is developed with least turn logic and a velocity controller based on a geometric method is designed with acceleration constraint to guarantee the formation keeping performance. In addition, a proportional derivative (PD) controller for acceleration is applied to smooth the velocity response of each vehicle. Finally, simulations of 5 UAVs in different situations are carried out to verify the effectiveness of the proposed method, both the trajectory tracking and formation keeping performance is as expected. © 2018 IEEE.
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Year: 2018
Page: 1275-1280
Language: English
Cited Count:
WoS CC Cited Count: 0
SCOPUS Cited Count: 4
ESI Highly Cited Papers on the List: 0 Unfold All
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Chinese Cited Count:
30 Days PV: 6
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