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Nominal motion control program in a supersonic carrier aircraft
- Authors: Balakin V.L.1, Potapov V.I.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 10, No 6 (2011)
- Pages: 15-21
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/2981
- DOI: https://doi.org/10.18287/2541-7533-2011-0-6(30)-15-21
- ID: 2981
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Abstract
A nominal program is suggested for controlling the aerodynamic lift coefficient in a supersonic carrier aircraft as the first stage of an aircraft-space system. The finite motion conditions at the given slope of the flight path are defined.
About the authors
V. L. Balakin
Samara State Aerospace University
Author for correspondence.
Email: balakin@ssau.ru
Doctor of technical sciences, professor
Head of the department of flight dynamics and control systems
V. I. Potapov
Samara State Aerospace University
Email: ssau@ssau.ru
Candidate of technical sciences
Assistant of the department of transportation organization and management
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