초록 ▼

A method of the invention allows the determination of aircraft sideslip using an air data probe and an inertial reference unit. A lateral sideslip component βLof the aircraft is calculated as a function of inertial flight information. An angular sideslip component βAof the aircraft is also calculate

A method of the invention allows the determination of aircraft sideslip using an air data probe and an inertial reference unit. A lateral sideslip component βLof the aircraft is calculated as a function of inertial flight information. An angular sideslip component βAof the aircraft is also calculated as a function of inertial flight information. The lateral sideslip component βLand the angular sideslip component βAare combined to obtain a total sideslip angle βTOTALfor the aircraft. The total sideslip angle βTOTALcan be used to compensate static pressure, angle of attack and other aircraft parameters for sideslip effects.

대표청구항 ▼

A method of the invention allows the determination of aircraft sideslip using an air data probe and an inertial reference unit. A lateral sideslip component βLof the aircraft is calculated as a function of inertial flight information. An angular sideslip component βAof the aircraft is also calculate

A method of the invention allows the determination of aircraft sideslip using an air data probe and an inertial reference unit. A lateral sideslip component βLof the aircraft is calculated as a function of inertial flight information. An angular sideslip component βAof the aircraft is also calculated as a function of inertial flight information. The lateral sideslip component βLand the angular sideslip component βAare combined to obtain a total sideslip angle βTOTALfor the aircraft. The total sideslip angle βTOTALcan be used to compensate static pressure, angle of attack and other aircraft parameters for sideslip effects. 9981200, Banez; US-5855128, 19990100, Voiculescu; US-5865044, 19990200, Wu; US-5870912, 19990200, Vito; US-5881587, 19990300, Vito; US-5887464, 19990300, Perez; US-5901586, 19990500, Hale; US-5906121, 19990500, Mankarious; US-5921115, 19990700, Winner; US-D412826, 19990800, Calpito; US-5996721, 19991200, Winner; US-6029483, 20000200, Daniels; US-6089055, 20000700, Vito; US-6116065, 20000900, Hale; US-D432390, 20001000, Geringer et al.; US-6131426, 20001000, Tarnofsky; US-6192724, 20010200, Vito; US-6202456, 20010300, Vickers; US-6212920, 20010400, Winner; US-6223568, 20010500, Wu; US-6223569, 20010500, Wu; US-6230527, 20010500, Wu; US-6240753, 20010600, Wu led "SYSTEM AND METHOD FOR TESTING A CIRCUIT IMPLEMENTED ON A PROGRAMMABLE LOGIC DEVICE" invented by Chakravarthy K. Allamsetty.