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公开(公告)号：US08386097B2
公开(公告)日：2013-02-26
申请号：US12046231
申请日：2008-03-11
IPC分类号： G05D1/00
CPC分类号： G05D1/0005 , G08G5/0052
摘要： Disclosed is a method and device for assisting guidance of an aircraft. A flight management system is used to determine guidance instructions that include speed instructions having at least one flight time constraint to guide the aircraft to a check-point. An accuracy level for complying with the flight time constraint and at least one error level for at least one flight parameter are generated by an accuracy generating unit. An operating margin for at least one second parameter is determined from the determined accuracy and error levels, with the operating margin being representative of air speed criterion values of the aircraft. A range determining unit is used to determine whether the range of air speed criterion values is within an air speed envelope of the aircraft, and the speed instructions are modified when the range of air speed criterion values is not within the air speed envelope.
摘要翻译： 公开了一种用于辅助飞机引导的方法和装置。 飞行管理系统用于确定包括具有至少一个飞行时间约束的速度指令的引导指令，以将飞机引导到检查点。 准确度生成单元产生用于符合飞行时间约束和至少一个飞行参数的至少一个误差水平的精度水平。 根据所确定的精度和误差水平来确定至少一个第二参数的操作裕度，其中操作裕度代表飞行器的空气速度标准值。 范围确定单元用于确定空中速度标准值的范围是否在飞行器的空气速度包络内，并且当空气速度标准值的范围不在空中速度包络内时，速度指令被修改。
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2.发明授权Method and device for servocontrolling an aircraft speed-wise in an approach phase 有权在接近阶段以速度方式伺服控制飞机的方法和装置公开(公告)号：US08352104B2
公开(公告)日：2013-01-08
申请号：US12617359
申请日：2009-11-12
IPC分类号： G06F19/00
CPC分类号： G08G5/02 , G05B19/416 , G05B2219/43036 , G05B2219/43074 , G05B2219/45071 , G05D1/0676
摘要： A method and device for servocontrolling an aircraft speed-wise in an approach phase. The device can adapt to the estimated time of passage of the aircraft at a particular point of the approach trajectory, the position of the start of deceleration of the aircraft in the approach phase.
摘要翻译： 一种用于在接近阶段中以飞行方式伺服控制飞机的方法和装置。 该装置可以适应飞行器在接近轨迹的特定点处的通过的估计时间，该飞行器在接近阶段的减速开始的位置。
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3.发明授权System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing 有权在进入跑道的过程中协助驾驶飞机的系统，以便着陆公开(公告)号：US07647140B2
公开(公告)日：2010-01-12
申请号：US11145951
申请日：2005-06-07
IPC分类号： G06F19/00
CPC分类号： G05D1/0676
摘要： A system for aiding the piloting of an aircraft during a runway approach includes an information source that provides information relating to the aircraft and its environment. A computation unit determines, with the aid of information provided by the information source, an energy reference profile having a trajectory reference profile and a speed reference profile that allows the aircraft to regain a stabilized approach trajectory, if it follows the reference profile. A monitor verifies that the aircraft is following the reference profile. An indicator supplies the pilot with piloting indications for piloting the aircraft so as to follow the reference profile.
摘要翻译： 在跑道方法中辅助飞机驾驶的系统包括提供与飞行器及其环境有关的信息的信息源。 计算单元借助于由信息源提供的信息确定具有轨迹参考轮廓和速度参考轮廓的能量参考轮廓，其允许飞机重新获得稳定的进场轨迹，如果它遵循参考轮廓。 监视器验证飞机是否遵循参考资料。 一个指示器为飞行员提供驾驶飞行员的驾驶指示，以便遵循参考资料。
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4.发明申请公开(公告)号：US20080103646A1
公开(公告)日：2008-05-01
申请号：US11877467
申请日：2007-10-23
CPC分类号： G08G5/0082 , G05D1/101 , G08G5/0039 , G08G5/025
摘要： The device 1 comprises means (3, 4, 5) making it possible to cause the aircraft to pass at least one particular waypoint of the flight trajectory, at an associated target time, and to do so to within an associated temporal tolerance.
摘要翻译： 设备1包括使得飞机能够在相关联的目标时间通过飞行轨迹的至少一个特定航点的装置（3,4,5），并且在相关联的时间容限内进行这种操作。
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公开(公告)号：US08027783B2
公开(公告)日：2011-09-27
申请号：US11934502
申请日：2007-11-02
IPC分类号： G06F19/00
摘要： An aircraft guidance device includes a flight computer that formulates all guidance orders for the aircraft, irrespective of a selected guidance mode.
摘要翻译： 飞机引导装置包括飞行计算机，其制定飞行器的所有指导命令，而不考虑所选择的引导模式。
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公开(公告)号：US07899586B2
公开(公告)日：2011-03-01
申请号：US12280126
申请日：2007-03-26
CPC分类号： G01C23/005
摘要： A guidance system includes a device to generate an alphanumeric identification characteristic, enabling identification of a data item which is used for a selected guidance mode of an aircraft. The system also includes a display unit which automatically shows the alphanumeric identification characteristic on a display screen.
摘要翻译： 引导系统包括用于产生字母数字识别特征的装置，使得能够识别用于飞行器的选定引导模式的数据项。 该系统还包括显示单元，其在显示屏幕上自动显示字母数字识别特性。
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公开(公告)号：US20100332111A1
公开(公告)日：2010-12-30
申请号：US11934502
申请日：2007-11-02
IPC分类号： G06F19/00
摘要： The guidance device (1) comprises a flight computer (7) which comprises means (15) for formulating all the guidance orders for the aircraft, irrespective of the guidance mode selected.
摘要翻译： 引导装置（1）包括飞行计算机（7），其包括用于为飞行器制定所有指导指令的装置（15），而不考虑所选择的引导模式。
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公开(公告)号：US20090259351A1
公开(公告)日：2009-10-15
申请号：US12422451
申请日：2009-04-13
CPC分类号： G05D1/0202
摘要： The device (1) comprises means (4) for determining speed setpoints making it possible to guide the aircraft so that it arrives at a particular waypoint at a time corresponding to a time constraint, by taking account of an upper speed limit for a current flight stretch and of an auxiliary upper speed limit for a distant flight stretch.
摘要翻译： 设备（1）包括用于确定速度设定点的装置（4），其使得可以引导飞机，使得其可以在与时间约束相对应的时间到达特定航点，通过考虑当前飞行的上限速度 拉伸和辅助上限极限为远距离飞行伸展。
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公开(公告)号：US08165734B2
公开(公告)日：2012-04-24
申请号：US12422451
申请日：2009-04-13
IPC分类号： G05D1/08
CPC分类号： G05D1/0202
摘要： Disclosed is a method and device of guiding an aircraft along a flight trajectory to comply with a time constraint for arriving at a required arrival time at a waypoint of the flight trajectory. Speed setpoints are determined according to a speed profile that complies with the required arrival time at the waypoint, based on estimated values of parameters relating to the flight of the aircraft, and by taking account of an upper limit for a maximum speed at which the aircraft flies along the flight trajectory. The determined speed setpoints are applied to the aircraft during guidance of the aircraft along the flight trajectory.
摘要翻译： 公开了一种沿着飞行轨迹引导飞行器的方法和装置，以符合在飞行轨迹的航点处达到所需到达时间的时间约束。 速度设定点根据速度曲线确定，该速度曲线符合航路点所需的到达时间，基于与飞机的飞行相关的参数的估计值，并考虑到飞行器的最大速度的上限 沿飞行轨迹飞行。 所确定的速度设定点在沿着飞行轨迹的飞行器引导期间被应用于飞行器。
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10.发明授权Method and device for aiding the piloting of an aircraft to prepare a phase of descent 有权协助驾驶飞机准备下降阶段的方法和装置公开(公告)号：US08150565B2
公开(公告)日：2012-04-03
申请号：US12256083
申请日：2008-10-22
IPC分类号： G05D1/00
CPC分类号： G05D1/0676
摘要： A method and device for aiding the piloting of an aircraft while respecting a time of arrival constraint at a first waypoint during a phase of descent. The method includes calculating an instant of arrival of the aircraft at an intermediate waypoint, in such a way that an estimated latest time of arrival at the first waypoint, corresponding to a minimum speed profile, occurs later by a predetermined first margin than the time of arrival constraint; determining a first speed profile between a current position of the aircraft and the intermediate waypoint, such that the intermediate waypoint is crossed at the calculated instant of arrival; determining a second speed profile, such that the first waypoint is crossed within the time of arrival constraint, starting from the intermediate waypoint at the calculated instant of arrival; and piloting the aircraft according to the first and then second speed profiles.
摘要翻译： 一种在下降阶段期间在第一航点考虑到抵达时间限制的同时辅助飞行员的驾驶的方法和装置。 该方法包括在中间航路点处计算飞行器的到达时刻，使得对应于最小速度分布的估计的到达第一航点的最近时间晚于相对于最小速度分布的预定的第一余量 到达约束; 确定飞机的当前位置和中间航点之间的第一速度轮廓，使得中间航点在所计算的到达时刻越过; 确定第二速度轮廓，使得在到达时间内的第一航路点在所计算的到达时刻从中间航点开始; 并根据第一和第二速度轮廓驾驶飞机。
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