CONTROL OF THE AIRCRAFT FLIGHT VELOCITY VECTOR BASED ON THE ENERGY APPROACH
Abstract
This paper presents a method of the aircraft flight velocity vector control synthesis taking into account constraints on the thrust of the power plant, the restriction is made on the basis of the use of the power triangle, representing an equilateral triangle whose height is interpreted as the thrust of the power plant. The control laws are synthesized based on the method of inverse dynamics problems.
About the Authors
V. P. Kharkov
ООО «Экспериментальная мастерская «НаукаСофт»
Russian Federation
Russian Federation
S. P. Khalyutin
ООО «Экспериментальная мастерская «НаукаСофт», МГТУ ГА
Russian Federation
Russian Federation
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Review
For citations:
Kharkov V.P., Khalyutin S.P. CONTROL OF THE AIRCRAFT FLIGHT VELOCITY VECTOR BASED ON THE ENERGY APPROACH. Civil Aviation High Technologies. 2015;(213):73-80. (In Russ.)
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