Method of terminal control in ascent segment of unmanned aerial vehicle with ballistic phase

Method of terminal control in ascent segment of unmanned aerial vehicle with ballistic phase

Introduction. The solution to the problem on the centroidal motion control synthesis (guidance problem) of an unmanned aerial vehicle (UAV) with long-range capabilities in the boost phase is considered. Control condition requires optimum fuel consumption. The principle of dynamic programming conside...

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Bibliographic Details
Main Authors: N. Y. Polovinchuk, S. V. Ivanov, M. Y. Zhukova, D. G. Belonozhko
Format: Article
Language:Russian
Published: Don State Technical University 2019-04-01
Series:Advanced Engineering Research
Subjects:
unmanned aerial vehicle (uav)
terminal guidance
direction cosines
pitching angle
angle of attack
boundary conditions
boost phase
ballistic flight phase.
Online Access:https://www.vestnik-donstu.ru/jour/article/view/1474
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