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1.发明申请公开(公告)号：US20100274418A1
公开(公告)日：2010-10-28
申请号：US12763880
申请日：2010-04-20
CPC分类号： G06Q20/00
摘要： A method for determining the quantity of fuel in an aircraft and an optimization criterion such as a cost index, notably used in an FMS, making it possible to maintain a time requirement of the RTA type, comprising a first step of computing the optimization criterion CIi as a function of the aircraft weight GWi-1 via a method of the RTA type and a second step of computing the weight of the aircraft GWi as a function of the optimization criterion Ci-1 computed in the first computation step and the aircraft weight GWi-1, executed by successive iterations, until the estimated flight time resulting from the computed parameters after the second computation step makes it possible to observe the time requirement to within a determined criterion δt, a last step determining the pair of values of aircraft weight GWand of performance criterion CIi-1 allowing an optimal fuel payload and the maintenance of the RTA.
摘要翻译： 一种用于确定飞行器中的燃料量的方法以及诸如成本指数的优化标准，特别是在FMS中使用的，使得可以维持RTA类型的时间需求成为可能，包括计算优化标准CIi的第一步骤 作为通过RTA类型的方法的飞机重量GWi-1的函数，以及第二步骤，根据在第一计算步骤中计算的优化准则Ci-1和飞行器重量GWi计算飞机GWi的权重 -1，直到由第二计算步骤之后的计算参数产生的估计飞行时间使得可以观察到在确定的标准δt内的时间要求，确定飞机重量值的一对值的最后步骤 的性能标准CIi-1允许最佳燃料有效载荷和RTA的维护。
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2.发明申请Method and Device for Optimizing the Deceleration Point of a Holding Circuit 审中-公开用于优化保持电路的减速点的方法和装置公开(公告)号：US20100324757A1
公开(公告)日：2010-12-23
申请号：US12821914
申请日：2010-06-23
CPC分类号： G05D1/0202
摘要： A method for optimizing the computation of the position of the braking point on the approach to a holding circuit for aircraft is provided. The method comprises computing the optimal position of the theoretical deceleration point allowing the aircraft to pass from its current speed to the maximum speed authorized at the entry point and of the theoretical deceleration distance, computing a trajectory portion forming a turn allowing the aircraft to enter the holding circuit and the position of the point of the start of the turn, computing a point for anticipating the turn, making it possible to take into account the banking rate of the aircraft, computing a margin, and computing the start-of-braking point, situated at a distance.
摘要翻译： 提供了一种用于优化在飞行器保持电路接近时制动点的位置计算的方法。 该方法包括计算理论减速点的最佳位置，允许飞机从当前速度通过到入口点授权的最大速度和理论减速距离，计算形成转弯的轨迹部分，允许飞机进入 保持电路和转弯点的位置，计算一个预期转弯点，有可能考虑到飞机的银行利率，计算边际和计算制动开始点 ，位于远处。
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3.发明申请公开(公告)号：US20080270022A1
公开(公告)日：2008-10-30
申请号：US12107868
申请日：2008-04-23
IPC分类号： G01C21/00
CPC分类号： G01C21/00 , G08G5/0034
摘要： The invention relates to a method for positioning reporting points that allows an exact positioning of the said reporting points on the track to be conserved, by continually using their original references in order to reposition these points each time the track is recalculated. The advantages of this solution are, on the one hand, to continually position the reporting points along the track rather than off the track and, thus, to locate the reporting points exactly notably in terms of distance, time and altitude.
摘要翻译： 本发明涉及一种用于定位报告点的方法，其允许通过不断地使用其原始参考来准确地定位要保存的轨道上的报告点，以便在每次重新计算轨道时重新定位这些点。 这个解决方案的优点是一方面不断地沿轨道定位报告点，而不是将轨迹定位，从而在距离，时间和高度方面确切地定位报告点。
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公开(公告)号：US20090234519A1
公开(公告)日：2009-09-17
申请号：US12400823
申请日：2009-03-10
申请人： Francois HOOFD , Emmanuel Dewas
发明人： Francois HOOFD , Emmanuel Dewas
IPC分类号： G06F19/00
CPC分类号： G08G5/0052 , G01C21/00 , G05D1/101 , G08G5/0039
摘要： The present invention relates to a trajectory calculation method making it possible to join a so-called military trajectory (Tm1) from a so-called civil trajectory (Tc1) and, reciprocally, to join a so-called civil trajectory (Tc2) from a so-called military trajectory (Tm1). For example, if the flight of an aircraft (A) must comply with civil standards over part of its flight plan and then perform a mission comprising tactical constraints before returning to a civil trajectory, the method described in the present patent application is entirely suitable.
摘要翻译： 轨迹计算方法本发明涉及一种轨迹计算方法，使得可以从所谓的民用轨迹（Tc1）连接所谓的军事轨迹（Tm1），并且相互地相互连接从所谓的民用轨迹（Tc2）到 所谓的军事轨迹（Tm1）。 例如，如果飞机（A）的飞行必须符合其飞行计划的一部分的民用标准，然后在返回到民用航迹之前执行包括战术约束的任务，则本专利申请中描述的方法是完全适用的。
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5.发明授权公开(公告)号：US08321072B2
公开(公告)日：2012-11-27
申请号：US12763880
申请日：2010-04-20
IPC分类号： G05D3/00
CPC分类号： G06Q20/00
摘要： A method for determining the quantity of fuel in an aircraft and an optimization criterion such as a cost index, notably used in an FMS, making it possible to maintain a time requirement of the RTA type, comprising a first step of computing the optimization criterion CIi as a function of the aircraft weight GWi-1 via a method of the RTA type and a second step of computing the weight of the aircraft GWi as a function of the optimization criterion Ci-1 computed in the first computation step and the aircraft weight GWi-1, executed by successive iterations, until the estimated flight time resulting from the computed parameters after the second computation step makes it possible to observe the time requirement to within a determined criterion δt, a last step determining the pair of values of aircraft weight GWi and of performance criterion CIi-1 allowing an optimal fuel payload and the maintenance of the RTA.
摘要翻译： 一种用于确定飞行器中的燃料量的方法以及诸如成本指数的优化标准，特别是在FMS中使用的，使得可以维持RTA类型的时间需求成为可能，包括计算优化标准CIi的第一步骤 作为通过RTA类型的方法的飞机重量GWi-1的函数，以及第二步骤，根据在第一计算步骤中计算的优化准则Ci-1和飞行器重量GWi计算飞机GWi的权重 -1，直到由第二计算步骤之后的计算参数产生的估计飞行时间使得可以观察到在确定的标准δt内的时间要求，确定飞机重量GWi的值的最后步骤 和性能标准CIi-1，允许最佳燃料有效载荷和RTA的维护。
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