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61. 发明公开

EP3101504A2 GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT 有权
标题翻译： GUST补偿的系统和方法飞机
公开(公告)号：EP3101504A2
公开(公告)日：2016-12-07
申请号：EP16172697.1
申请日：2016-06-02
申请人： The Boeing Company
发明人： ABDEL-MOTAGALY, Khaled , CAICEDO, Rafael E. , DALLARA, Christopher D. , HO, Alexander C. , KIOUMARS, Najmabadi , SIU, Tze L. , STREFLING, Paul C. , YAMASHIRO, Hisako
IPC分类号： G05D1/04 , B64C13/16
CPC分类号： G05D1/0825 , B64C13/16 , B64C13/18 , B64D2700/62228 , G05D1/0066
摘要： A gust compensation system 200 is configured to adaptively reduce gust loads exerted into an aircraft 100/500. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft 100. The first sensor 110 is configured to output a first signal. A second sensor 120 may be distally located from the front of the aircraft 100. The second sensor 120 is configured to output a second signal. A gust signal sub-system 202 is configured to receive the first and second signals and generate a gust signal 226 based on analysis of the first and second signals. The gust signal sub-system 202 outputs the gust signal 226 and may modify a load parameter signal 220 in response to the gust signal 226 exceeding a load alleviation threshold.

62. 发明授权

EP2403757B1 UNMANNED AIR VEHICLE (UAV), CONTROL SYSTEM AND METHOD 有权
标题翻译：无人驾驶飞机（UAV），控制系统和方法
公开(公告)号：EP2403757B1
公开(公告)日：2014-04-16
申请号：EP10722158.2
申请日：2010-03-05
申请人： Cranfield Aerospace Ltd
发明人： THOMASSON, Peter, Geoffrey , JONES, Robert, Idris , POLL, David, Ian, Alistair
IPC分类号： B64C13/16
CPC分类号： B64C39/024 , B64C2201/028 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G05D1/0094 , G05D1/0825

63. 发明授权

EP1449743B1 Vehicle motion model generating device and method for generating vehicle motion model 有权
标题翻译：装置和方法用于产生车辆运动模型
公开(公告)号：EP1449743B1
公开(公告)日：2013-04-10
申请号：EP04003553.7
申请日：2004-02-17
申请人： Fuji Jukogyo Kabushiki Kaisha
发明人： Tsuyoshi, Torii , Itaru, Seta
IPC分类号： G06N3/04 , B62D6/00 , G05B13/02
CPC分类号： G06N3/0454 , B60G17/0162 , B60G17/0182 , B60G17/0195 , B60G2400/0521 , B60G2400/0522 , B60G2400/0523 , B60G2400/104 , B60G2400/106 , B60G2400/204 , B60G2400/41 , B60G2400/42 , B60G2400/44 , B60G2600/1877 , B60G2600/1878 , B60G2800/012 , B60G2800/24 , B60G2800/70 , B60G2800/90 , B60T8/174 , B60T2270/86 , B60W2050/0057 , B62D6/00 , G05B13/027 , G05B17/02 , G05D1/0825

64. 发明授权

EP2065777B1 Robust control effector allocation 有权
标题翻译：强大的分配控制执行器
公开(公告)号：EP2065777B1
公开(公告)日：2012-10-17
申请号：EP08075881.6
申请日：2008-11-14
申请人： The Boeing Company
发明人： Lavretsky, Eugene , Diecker, Ryan D. , Brinker, Joseph S.
IPC分类号： G05D1/08
CPC分类号： G05D1/0825

65. 发明授权

EP1429220B2 Method and computer program product for controlling the control effectors of an aerodynamic vehicle 有权
标题翻译：用于控制控制表面，用于空气动力学车辆的方法和计算机程序产品
公开(公告)号：EP1429220B2
公开(公告)日：2012-09-12
申请号：EP03078799.8
申请日：2003-12-02
申请人： The Boeing Company
发明人： Musgrave, Jeffrey L. , Jones, Richard D.
IPC分类号： G05D1/08 , G05B13/02
CPC分类号： G05B13/024 , G05D1/0825

66. 发明公开

EP2065777A3 Robust control effector allocation 有权
标题翻译：强大的分配控制执行器
公开(公告)号：EP2065777A3
公开(公告)日：2010-08-04
申请号：EP08075881.6
申请日：2008-11-14
申请人： The Boeing Company
发明人： Lavretsky, Eugene , Diecker, Ryan D. , Brinker, Joseph S.
IPC分类号： G05D1/10
CPC分类号： G05D1/0825
摘要： Method and apparatus is disclosed which allocates the execution of a commanded vehicle maneuver among the vehicle's control effectors capable of affecting such maneuver, with consideration given to the possible nonlinear and/or non-monotonic effects each control effector's displacement may have on the vehicle and on each other's performance.

67. 发明公开

EP1766332A4 SYSTEMS AND METHODS FOR ESTIMATING POSITION, ATTITUDE, AND/OR HEADING OF A VEHICLE 审中-公开
标题翻译：系统和方法来估计位置的位置和/或运动的车辆的方向
公开(公告)号：EP1766332A4
公开(公告)日：2010-03-03
申请号：EP05758536
申请日：2005-06-02
申请人： ATHENA TECHNOLOGIES INC
发明人： VOS DAVID WILLIAM , GAVRILETS VLADISLAV
IPC分类号： G01C21/16 , G05D1/08
CPC分类号： G05D1/0825 , G01C21/165

68. 发明授权

EP1844376B1 PROCEDE ET DISPOSITIF DE PILOTAGE D'UN AVION EN TANGAGE 有权
标题翻译：方法和装置飞行饲养飞机
公开(公告)号：EP1844376B1
公开(公告)日：2008-12-03
申请号：EP06709204.9
申请日：2006-01-31
申请人： AIRBUS France
发明人： DELANNOY, Stéphane
IPC分类号： G05D1/08
CPC分类号： G05D1/0825
摘要： The invention relates to a method and device for piloting a pitching aircraft. The inventive device (1) comprises: means (4) for receiving an ordered load factor (NZc); means (11) for estimating a load factor (NZcg) that is applied to the aircraft; a means (12) for calculating a control order for a means (5) for deflecting a control surface (7) of the aircraft, taking account of at least the following expression K1.NZc + K2.NZcg, K1 and K2 representing gain values; means (13) for determining the Mach number; means (14) for determining the angle of incidence; means (15) for comparing the angle of incidence with a reference value; and means (16) for determining a modified gain value (?K2) with the aid of the Mach number and the angle of incidence if said angle of incidence is greater than the reference value, said modified gain value (?K2) replacing gain value K2 in the calculation performed by the calculation means (12).

69. 发明公开

EP1656597A1 INTELLIGENT DATABASE FOR PERFORMANCE PREDICTIONS 有权转让
标题翻译：飞行员和飞行员阵容
公开(公告)号：EP1656597A1
公开(公告)日：2006-05-17
申请号：EP04781714.3
申请日：2004-08-20
申请人： Honeywell International Inc.
发明人： HARTMANN, Gary, L. , PRATT, Stephen, G. , OLAUGHLIN, Brian, E.
IPC分类号： G05D1/00 , G05D1/08
CPC分类号： G05D1/0005 , G05D1/0825
摘要： The accuracy of flight management systems, based on mathematical prediction models calculated from aircraft specific data, are improved by adding engine sensor data to the calculations, checking sensor and pilot entered data, and comparing data measured from redundant sensors. A thrust estimate, calculated from available engine sensors (20-22, 26) is added to the thrust-minus-drag aircraft model allowing prediction parameters to be accurately calculated even in a cruise condition. Sensor data and pilot entered data used in calculating predication parameters are checked to improve accuracy. Redundant sensor data is compared to determine the level of agreement. Redundant sensor data is also compared with a valid data range to find the sensor with the most accurate data.
摘要翻译：通过将发动机传感器数据添加到计算，检查传感器和飞行员输入的数据，以及比较从冗余传感器测量的数据，可以改进飞行管理系统基于从飞机特定数据计算的数学预测模型的准确性。从可用的发动机传感器计算出的推力估计值被加到推力减阻飞行器模型中，即使在巡航条件下也能够准确地计算预测参数。检查用于计算预测参数的传感器数据和导频输入数据，以提高精度。比较冗余传感器数据以确定协议级别。还将冗余传感器数据与有效数据范围进行比较，以找到具有最准确数据的传感器。

70. 发明授权

EP1312998B1 Procédé et dispositif pour déterminer en temps réel le comportement d'un mobile, en particulier d'un aéronef 有权
标题翻译：用于实时确定车辆的行为，特别是飞行器的方法和装置
公开(公告)号：EP1312998B1
公开(公告)日：2006-01-11
申请号：EP02292412.0
申请日：2002-10-01
申请人： EUROCOPTER
发明人： Eglin, Paul
IPC分类号： G05D1/08
CPC分类号： G05D1/0825

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