Optimal Fuel Consumption Trajectories of a Civil Supersonic Aircraft

Optimal Fuel Consumption Trajectories of a Civil Supersonic Aircraft

The optimal fuel consumption trajectories of a supersonic passenger aircraft are constructed. A mathematical model of an airliner, which describes in detail the properties of the device related to the design characteristics of the aircraft, is applied. For optimization, the preliminary division of t...

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Bibliographic Details
Published in:Journal of computer & systems sciences international Vol. 61; no. 4; pp. 664 - 676
Main Authors: Kumakshev, S. A., Shmatkov, A. M.
Format: Journal Article
Language:English
Published: Moscow Pleiades Publishing 01-08-2022
Springer Nature B.V
Subjects:
Aircraft design
Control
Control Systems for Moving Objects
Dynamic programming
Engineering
Fuel consumption
Mechatronics
Optimization
Passenger aircraft
Robotics
Supersonic aircraft
Trajectories
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Summary:The optimal fuel consumption trajectories of a supersonic passenger aircraft are constructed. A mathematical model of an airliner, which describes in detail the properties of the device related to the design characteristics of the aircraft, is applied. For optimization, the preliminary division of the trajectory into separate sections followed by the assembly of the optimal solution from them is not used. The whole flight is considered as a single process. The classical method of dynamic programming is used for the calculations.
ISSN:1064-2307
1555-6530
DOI:10.1134/S1064230722040128