Email this article Aircraft Trajectory Control at the Motion on the Predetermined Route Based on the Global Navigation Satellite System
- Authors: Erokhin V.V.1
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Affiliations:
- Irkutsk Branch of Moscow State Technical University of Civil Aviation
- Issue: Vol 61, No 3 (2018)
- Pages: 371-378
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230590
- DOI: https://doi.org/10.3103/S106879981803008X
- ID: 230590
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Abstract
An algorithm to control the aircraft trajectory is proposed. This algorithm is based on the dynamic stochastic systems optimal control theory. The optimal control implementation is shown to reduce the deviation of the controlled trajectory from the predetermined one. The optimal control is based on estimating phase coordinates with the high accuracy by the global navigation satellite system.
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About the authors
V. V. Erokhin
Irkutsk Branch of Moscow State Technical University of Civil Aviation
Author for correspondence.
Email: Ww_erohin@mail.ru
Russian Federation, ul. Kommunarov 3, Irkutsk, 664047
