Abstract | ||
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We present a formation flight control strategy featuring a collision avoidance scheme. The control algorithm is based on a Sliding Mode controller. The controller sliding surfaces account for aircraft maneuvering limitations, restricting the required velocities to a feasible set. Further, the relative position between vehicles affects the sliding surfaces shape, enabling collision avoidance. The control method derivation is based on an extended unicycle model, resulting in a controller adequate for fixed wing aircraft. |
Year | DOI | Venue |
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2011 | 10.1109/CDC.2011.6160637 | 2011 50TH IEEE CONFERENCE ON DECISION AND CONTROL AND EUROPEAN CONTROL CONFERENCE (CDC-ECC) |
Keywords | Field | DocType |
vehicle dynamics,atmospheric modeling,shape | Control algorithm,Control theory,Wing,Control theory,Computer science,Collision,Control engineering,Atmospheric model,Feasible region,Vehicle dynamics | Conference |
ISSN | Citations | PageRank |
0743-1546 | 0 | 0.34 |
References | Authors | |
0 | 4 |
Name | Order | Citations | PageRank |
---|---|---|---|
Ricardo Bencatel | 1 | 0 | 1.35 |
Mariam Faied | 2 | 14 | 4.67 |
João B. Sousa | 3 | 62 | 8.87 |
Anouck R. Girard | 4 | 135 | 20.51 |