A system and method for estimating a plurality of airspeed parameters of an aircraft is disclosed. The system comprises one or more processors and a memory coupled to the processor. The memory storing data comprising a database and program code that, when executed by the one or more processors, causes the system to receive a plurality of operating parameters that each represent an operating condition of the aircraft. The system is further caused to determine a model based dynamic pressure based on the operating parameters. The model based dynamic pressure is estimated based on steady flight conditions of the aircraft. The system is further caused to determine a bridge based dynamic pressure based on at least a temperature deviation and an inertial speed vector. The bridge based dynamic pressure is estimated for extreme flight conditions of the aircraft.
СИСТЕМА ОЦЕНКИ ВОЗДУШНОЙ СКОРОСТИ ЛЕТАТЕЛЬНОГО АППАРАТА НА ОСНОВАНИИ МОДЕЛИ НАКОПЛЕНИЯ ДАННЫХ О ПОГОДЕ.
2019-08-26
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |
СИСТЕМА ОЦЕНКИ ВОЗДУШНОЙ СКОРОСТИ ЛЕТАТЕЛЬНОГО АППАРАТА НА ОСНОВАНИИ МОДЕЛИ ЛОБОВОГО СОПРОТИВЛЕНИЯ
European Patent Office | 2019
European Patent Office | 2017