-
公开(公告)号：US08010288B2
公开(公告)日：2011-08-30
申请号：US11719134
申请日：2005-11-10
IPC分类号： G08G11/16
CPC分类号： G08G5/045 , G08G5/0086
摘要： An aircraft terrain avoidance system include a device having a first unit knowing a profile of the terrain that is located at the front of the aircraft, a second unit for determining an avoidance trajectory, a third unit which is connected to the first and second units and used to verify if there is a terrain collision risk for the aircraft, a fourth unit for emitting an alarm signal in the event of detection of a collision risk by the third unit, at least one aircraft performance database relating to an avoidance maneuvering gradient which can be flown by the aircraft according to particular flight parameters, and a fifth unit for determining the effective values of the particular parameters during the flight of the aircraft. The third unit is formed such that it is possible to determine the avoidance trajectory according to information received from the database and the fifth unit.
摘要翻译： 飞机地形回避系统包括具有第一单元的设备，该第一单元知道位于飞机前面的地形的轮廓，用于确定回避轨迹的第二单元，连接到第一和第二单元的第三单元，以及 用于验证飞机是否存在地形碰撞风险;第四单元，用于在检测到第三单元的碰撞风险的情况下发出报警信号;至少一个与回避机动梯度有关的飞机性能数据库，其可以 根据特定飞行参数由飞行器飞行，以及用于确定飞行器飞行期间的特定参数的有效值的第五单元。 第三单元形成为能够根据从数据库和第五单元接收的信息来确定回避轨迹。
-
公开(公告)号：US20090076728A1
公开(公告)日：2009-03-19
申请号：US11719134
申请日：2005-11-10
CPC分类号： G08G5/045 , G08G5/0086
摘要： The device (1) comprises a first means (2) knowing the profile of the terrain at least that which is located at the front of the aircraft, a second means (3) for determining an avoidance trajectory, a third means (4) which is connected to the first and second means (2, 3) and used to verify if there is a terrain collision risk for the aircraft, a fourth means (7) for emitting an alarm signal in the event of detection of a collision risk by the third means (4), at least one aircraft performance data base (Bi) relating to an avoidance maneuvering gradient which can be flown by the aircraft according to particular flight parameters, and a fifth means (9) for determining the effective values of the particular parameters during the flight of the aircraft, wherein the third means (3) is formed in such a way that it is possible to determine the avoidance trajectory according to the information received from the data base (Bi) and the fifth means (9).
摘要翻译： 所述装置（1）包括第一装置（2），所述第一装置（2）至少知道位于所述飞行器前部的所述地形轮廓，用于确定回避轨迹的第二装置（3），第三装置 连接到第一和第二装置（2,3），并用于验证飞机是否存在地形碰撞风险;第四装置（7），用于在检测到碰撞风险的情况下发出报警信号 第三装置（4），与飞机根据特定飞行参数可飞行的回避机动梯度有关的至少一个飞机性能数据库（Bi）以及用于确定特定飞行参数的有效值的第五装置（9） 飞行器飞行期间的参数，其中第三装置（3）形成为可以根据从数据库（Bi）和第五装置（9）接收的信息来确定回避轨迹。
-
公开(公告)号：US07283895B2
公开(公告)日：2007-10-16
申请号：US11047654
申请日：2005-02-02
申请人： Christophe Bouchet
发明人： Christophe Bouchet
IPC分类号： B64C1/00
CPC分类号： G05D1/0202 , G01C21/12 , G08G5/00 , G08G5/0052
摘要： A method and device for calculating a target speed of an aircraft may include a flight point time determining section that determines when the aircraft actually gets to a particular flight point, taking account of the aircraft's current target speed. A time interval calculating section calculates a time interval between the predetermined time at which the aircraft must get to the particular flight point and the determined actual time. A speed updating section updates the target speed and applies the updated target speed to the aircraft if the calculated time interval is greater than a duration of comparison, which is variable and depends on the actual distance so as to decrease when the actual distance decreases.
摘要翻译： 用于计算飞行器的目标速度的方法和装置可以包括飞行点时间确定部分，其确定飞机何时实际到达特定飞行点，考虑飞机的当前目标速度。 时间间隔计算部分计算飞机必须到达特定飞行点的预定时间与确定的实际时间之间的时间间隔。 如果所计算的时间间隔大于比较的持续时间，则速度更新部分更新目标速度并将更新的目标速度应用于飞行器，该持续时间是可变的，并且取决于实际距离，以便在实际距离减小时减小。
-
14.发明申请公开(公告)号：US20120253562A1
公开(公告)日：2012-10-04
申请号：US13422031
申请日：2012-03-16
IPC分类号： G05D1/04
CPC分类号： G08G5/0034 , G01C21/20 , G01C23/005 , G05D1/0202 , G08G5/0039
摘要： The device includes means for determining a plurality of successive standard flight sections (S1A, S2A, S3A, S4A) comprising a level and a transition phase for reaching this level, and means for joining together these successive flight sections (S1A, S2A, S3A, S4A) in order to form the vertical profile (PV1) of the flight plan.
摘要翻译： 该装置包括用于确定多个连续的标准飞行段（S1A，S2A，S3A，S4A）的装置，其包括用于达到该水平的水平和过渡阶段，以及用于将这些连续飞行段（S1A，S2A，S3A， S4A），以形成飞行计划的垂直剖面（PV1）。
-
公开(公告)号：US08155866B2
公开(公告)日：2012-04-10
申请号：US12422542
申请日：2009-04-13
IPC分类号： G06F19/00
CPC分类号： G05D1/0202 , G08G5/0039 , G08G5/0052
摘要： Disclosed is a method and device for guiding an aircraft flying along a flight trajectory. The flight trajectory has at least one constrained section, and the aircraft flies at a required speed within the constrained section to comply with a required arrival time at a predetermined waypoint in the constrained section. Auxiliary speed setpoints are determined to guide the aircraft to arrive at an auxiliary arrival tune at an auxiliary waypoint, with the auxiliary speed setpoints being applied by a guidance system to guide the aircraft.
摘要翻译： 公开了一种用于引导飞行器沿飞行轨迹飞行的方法和装置。 飞行轨迹具有至少一个约束部分，并且飞机以受限部分内的所需速度飞行，以符合约束部分中预定航路点处的所需到达时间。 确定辅助转速设定值以引导飞机在辅助通路点处到达辅助到达曲线，辅助转速设定点由引导系统施加以引导飞行器。
-
16.发明授权Device for constructing and securing a low altitude flight plan path intended to be followed by an aircraft 有权用于构建和确保飞机遵循的低空飞行计划路线的装置公开(公告)号：US07765036B2
公开(公告)日：2010-07-27
申请号：US11672393
申请日：2007-02-07
申请人： Christophe Bouchet
发明人： Christophe Bouchet
IPC分类号： G01C23/00
CPC分类号： G08G5/006 , G01C21/00 , G08G5/0021 , G08G5/0034
摘要： A device for constructing and securing a low altitude flight path intended to be followed by an aircraft. The device includes a first processing unit which has a Design Assurance Level (DAL) C requirement level and which determines a low altitude flight path, using data coming from a first database qualified according to a Data Process Assurance Level (DPAL) 2 standard, and a second processing unit which has a DAL A requirement level and which checks the flight path determined by said first processing unit, using data corning from a second database qualified according to a DPAL1 standard.
摘要翻译： 一种用于构造和固定旨在由飞机跟随的低空飞行路径的装置。 该设备包括具有设计保证等级（DAL）C要求级别并且使用来自根据数据处理保证级别（DPAL）2标准认证的第一数据库的数据确定低空飞行路径的第一处理单元，以及 具有DAL A要求等级的第二处理单元，并且使用从根据DPAL1标准认证的第二数据库进行校正的数据来检查由所述第一处理单元确定的飞行路径。
-
17.发明授权Method and device for automatically managing the vertical profile of the flight plan of an aircraft 有权用于自动管理飞机飞行计划垂直剖面的方法和装置公开(公告)号：US08812180B2
公开(公告)日：2014-08-19
申请号：US13422031
申请日：2012-03-16
CPC分类号： G08G5/0034 , G01C21/20 , G01C23/005 , G05D1/0202 , G08G5/0039
摘要： The vertical profile management device includes a flight management system unit that selects a plurality of successive standard cruise sections, each comprising a level phase and a transition phase. The cruise sections are defined by a plurality of features, including waypoints corresponding to a section starting point and a section ending point, a transition type, a transition mode, a transition speed, a level altitude, and a level speed. The flight management system unit also joins together the successive cruise sections in order to form a vertical profile of a flight plan. The cruise sections are configured to be added, removed, or re-sequenced in the flight plan because each section ending point is configured to be the section starting point of a next cruise section in the series.
摘要翻译： 垂直剖面管理装置包括飞行管理系统单元，其选择多个连续的标准巡航区段，每个巡航区段包括水平阶段和过渡阶段。 巡航部分由多个特征限定，包括对应于部分起点和截面终点，过渡类型，转变模式，转变速度，水平高度和等级速度的航点。 飞行管理系统单元还将连续的巡航部分连接在一起，以形成飞行计划的垂直轮廓。 巡航部分配置为在飞行计划中添加，删除或重新排序，因为每个截面的终点都被配置为系列中下一个巡航部分的部分起始点。
-
公开(公告)号：US20050216140A1
公开(公告)日：2005-09-29
申请号：US11047654
申请日：2005-02-02
申请人： Christophe Bouchet
发明人： Christophe Bouchet
CPC分类号： G05D1/0202 , G01C21/12 , G08G5/00 , G08G5/0052
摘要： The device (1) comprises means (2) for determining the actual time at which the aircraft gets to a particular flight point, taking account of a current target speed, means (3) for calculating a time interval defined between the predetermined time at which the aircraft must get to the particular flight point and said actual time, means (5) for comparing this time interval with a duration of comparison, means (7) for updating the target speed, which is applied to the aircraft, if this time interval is greater than the duration of comparison, means (10) for determining the actual distance between the current position of the aircraft and the particular flight point, and means (11) for determining said duration of comparison which is variable and which depends on the actual distance in such a way as to decrease when the actual distance decreases.
摘要翻译： 装置（1）包括用于确定飞机到达特定飞行点的实际时间的装置（2），考虑当前目标速度，用于计算在预定时间之间定义的时间间隔的装置（3） 飞机必须到达特定飞行点并说实际时间，这意味着（5）用于将该时间间隔与比较持续时间进行比较，意味着（7）用于更新应用于飞机的目标速度，如果该时间间隔 大于比较持续时间，用于确定飞行器的当前位置与特定飞行点之间的实际距离的装置（10）以及用于确定所述比较持续时间的装置（11），所述持续时间是可变的，并且取决于实际 以实际距离减小的方式减小距离。
-
-
-
-
-
-
-
搜索结果
18 条记录 (耗时 0.02 秒)
