Optimal Control of Hypersonic Planning Maneuvers Based on Pontryagin’s Maximum Principle

Optimal Control of Hypersonic Planning Maneuvers Based on Pontryagin’s Maximum Principle

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The work objective is the synthesis of simple analytical formula of the optimal roll angle of hypersonic gliding vehicles for conditions of quasi-horizontal motion, allowing its practical implementation in onboard control algorithms.The introduction justifies relevance, formulates basic control task...

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Bibliographic Details
Main Author: A. Yu. Melnikov
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2016-06-01
Series:Aèrokosmičeskij Naučnyj Žurnal
Subjects:
algorithm
aerospace system
control
hypersonic
gliding vehicle
roll
criterion
optimization
maximum principle
hamiltonian
mated parameters
trajectory
maneuver
flight
atmosphere
Online Access:https://aerospace.elpub.ru/jour/article/view/26

Internet

https://aerospace.elpub.ru/jour/article/view/26

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