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The task of hypersonic aircraft motion optimum control at the acceleration – climb stage in the atmosphere
- Authors: Bebyakov A.A.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 6, No 1 (2007)
- Pages: 15-21
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/474
- DOI: https://doi.org/10.18287/2541-7533-2007-0-1(12)-15-21
- ID: 474
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Abstract
The task of optimum control of the hypersonic aircraft centre of mass on the condition of minimum fuel consumption is dealt with using the maximal principle method.
About the authors
A. A. Bebyakov
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
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