Comparison of hypersonic aircraft quasi horizontal maneuver control methods
Authors: Kalinovskiy T.A. | |
Published in issue: #1(1)/2016 | |
DOI: 10.18698/2541-8009-2016-1-10 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control |
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Keywords: hypersonic aircraft, control method, maneuvering, banking angle, atmosphere, optimal control |
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Published: 06.09.2016 |
We studied the movement and possible maneuvering of the advanced hypersonic aircraft in the Earth's atmosphere. We solved the problem of determining the maximum capacity of the system, the quality assessment of the control algorithms by comparing the calculated trajectory with the optimal (reference) one.
References
[1] Nesterenko G.N. Kosmicheskaya aviatsiya [Space aviation]. Moscow, VI Publ., 1969. 60 p. (in Russ.).
[2] Mel’nikov A.Yu. Optimal’noe upravlenie manevrami giperzvukovogo planera na osnove printsipa maksimuma Pontryagina [Optimum control on hypervelocity glider evolution using Pontryagin’s maximum principle]. Moscow, Bauman MSTU Publ., 2015. 14 p. (in Russ.).
[3] Pyshnov V.S. Polet s bol’shimi dokosmicheskimi skorostyami [High pre-space speed flight]. Zhukovsky VVIA Publ., 1959. 59 p. (in Russ.).
[4] Koryanov V.V., Kazakovtsev V.P. Osnovy teorii kosmicheskogo poleta. Ch. 1. [Space flight fundamentals. Part 1]. Moscow, Bauman MSTU Publ., 2013. 27 p. (in Russ.).
[5] James M. Acton. Hypersonic boost-glide weapons. Science and Global Security, 2015, vol. 23, no. 3, pp. 191-219.