This paper researches optimization maneuver strategy of UAV after engine stopped to make the loss of height of UAV minimum. Research has been done in two conditions, unpowered balanced glide straight flight and unpowered balanced glide turn maneuver. In this paper, the angle of attack and angle of roll has been given in order to make sure that the loss of the height is a minimum. The results of the simulations show that the optimization maneuver strategy in this paper is correct.
Optimization Maneuver Strategy which Make the Loss of Height of UAV Minimum after Engine Stopped
Applied Mechanics and Materials ; 668-669 ; 619-624
2014-10-08
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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