Trajectory control of a high altitude hypervelocity flying vehicle in the midcourse active phase of the flight
| Autor: | K. I. Sypalo, V. L. Miroshkin, A. I. Kibzun, M. N. Krasil'shchikov |
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| Rok vydání: | 2013 |
| Předmět: |
Computer Networks and Communications
Angle of attack business.industry Applied Mathematics Robotics Thrust Aerodynamics Effects of high altitude on humans Theoretical Computer Science Aerodynamic force Altitude Control and Systems Engineering Physics::Space Physics Hypervelocity Environmental science Astrophysics::Earth and Planetary Astrophysics Computer Vision and Pattern Recognition Artificial intelligence Aerospace engineering business Physics::Atmospheric and Oceanic Physics Software Information Systems |
| Zdroj: | Journal of Computer and Systems Sciences International. 52:628-636 |
| ISSN: | 1555-6530 1064-2307 |
| DOI: | 10.1134/s1064230713040102 |
| Popis: | An approach to the control of the motion of the center of mass of a high altitude hypervelocity flying vehicle whose engine thrust and aerodynamics strongly depend on the angle of attack in the midcourse active phase of the flight is proposed. This approach provides a basis for the method of the trajectory control of motion. The motion of this flying vehicle is simulated with regard to the disturbed atmosphere. It is shown that the proposed approach can be used to form launching zones of high altitude hypervelocity flying vehicles. |
| Databáze: | OpenAIRE |
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