Мақаланы E-mail арқылы жіберу Aircraft Trajectory Control at the Motion on the Predetermined Route Based on the Global Navigation Satellite System
- Авторлар: Erokhin V.1
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Мекемелер:
- Irkutsk Branch of Moscow State Technical University of Civil Aviation
- Шығарылым: Том 61, № 3 (2018)
- Беттер: 371-378
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
Аннотация
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.
Негізгі сөздер
Авторлар туралы
V. Erokhin
Irkutsk Branch of Moscow State Technical University of Civil Aviation
Хат алмасуға жауапты Автор.
Email: Ww_erohin@mail.ru
Ресей, ul. Kommunarov 3, Irkutsk, 664047
