IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0336730
(2003-01-06)
|
우선권정보 |
FR-0004334 (2002-04-08) |
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
Stevens, Davis, Miller & Mosher, LLP
|
인용정보 |
피인용 횟수 :
6 인용 특허 :
6 |
초록
▼
According to the invention, in this aircraft, the elements of the inertial reference system are separated according to whether they are intended for navigation (CI) or flight control (5, 6, 7). The accelerometers (5 and 6) intended for flight control are arranged at a vibration antinode, while the g
According to the invention, in this aircraft, the elements of the inertial reference system are separated according to whether they are intended for navigation (CI) or flight control (5, 6, 7). The accelerometers (5 and 6) intended for flight control are arranged at a vibration antinode, while the gyrometers (7) dedicated to flight control are placed at a vibration node. The accelerometers (5 and 6) and the gyrometers (7) are connected to the flight control computer (12) and their measurements serve as flight control parameters.
대표청구항
▼
According to the invention, in this aircraft, the elements of the inertial reference system are separated according to whether they are intended for navigation (CI) or flight control (5, 6, 7). The accelerometers (5 and 6) intended for flight control are arranged at a vibration antinode, while the g
According to the invention, in this aircraft, the elements of the inertial reference system are separated according to whether they are intended for navigation (CI) or flight control (5, 6, 7). The accelerometers (5 and 6) intended for flight control are arranged at a vibration antinode, while the gyrometers (7) dedicated to flight control are placed at a vibration node. The accelerometers (5 and 6) and the gyrometers (7) are connected to the flight control computer (12) and their measurements serve as flight control parameters. P; 1993-234899, JP; 1993-235047, JP; 1993-251339, JP; 1993-270997, JP; 1993-283336, JP; 1993-291152, JP; 1993-304334, JP; 1993-343327, JP; 1993-343685, JP; 1994-045606, JP; 1994-132236, JP; 1994-177381, JP; 1994-196809, JP; 1994-222388, JP; 1994-224138, JP; 1994-230421, JP; 1994-252057, JP; 1994-291048, JP; 1995-070752, JP; 1995-086269, JP; 1996-181076, JP; 1996-245291, JP; 1996-264530, JP; 1997-260786, JP; 1997-293681, JP; 1998-188840, JP; 1998-308283, JP; 1999-269652, JP; 2000-031387, JP; 2000-058777, JP; 2000-068072, JP; 2000-087029, JP; 2000-319772, JP; 2000-138094, JP; 2000-218445, JP; 2000-319772, JP; 2000-340883, JP; 2000-353666, JP; 2001-020075, JP; 2001-62244, JP; 2001-152339, JP; 2001-172767, JP; 2001-189312, JP; 2001-217206, JP; 2001-220287, JP; 2001-220294, JP; 2001-240972, JP; 2001-254181, JP; 2001-284042, JP; 2001-303251, JP; 2001-328900, JP; WO90/002216, WO; WO91/010510, WO; WO93/002111, WO; WO96/018756, WO; WO96/171070, WO; WO98/006889, WO; WO98/051838, WO; WO99/001595, WO; WO99/013504, WO; WO99/029924, WO; WO99/041423, WO; WO99/065064, WO; 00/11721, WO; 00/15865, WO; 00/15881, WO; 00/16377, WO; 00/54320, WO; 00/63957, WO; WO00/79019, WO; 00/79019, WO; 00/79576, WO; 01/15220, WO; 01/15220, WO; 01/17692, WO; 01/27346, WO; 01/27347, WO; 01/29280, WO; 01/29891, WO; 01/29893, WO; 01/36702, WO; 01/40541, WO; 01/66832, WO; 02/08488, WO
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