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1.发明授权Method and device for an optimal management of the vertical trajectory of an aircraft 有权用于最佳管理飞行器垂直轨迹的方法和装置公开(公告)号：US08892275B2
公开(公告)日：2014-11-18
申请号：US13559295
申请日：2012-07-26
申请人： Florian Constans , Mickael Lefebvre
发明人： Florian Constans , Mickael Lefebvre
CPC分类号： G08G5/025 , G05D1/0005 , G05D1/0676
摘要： A method and device optimize the vertical trajectory of an aircraft in flight along a predetermined approach trajectory. The method and device include the use of a calculator, which is structured to predict a predicted stabilization altitude at which the aircraft will reach a setpoint approach speed as a function of the current aircraft parameter values, a theoretical vertical trajectory, and predetermined models of aerodynamic efficiency of the aircraft. A comparator is structured to determine absolute value differences between the predicted stabilization altitude and the setpoint stabilization altitude and to compare the differences against a predetermined altitude threshold. A vertical trajectory determination unit is structured to determine an optimized vertical trajectory as a function of the current aircraft parameter values, auxiliary parameter values corresponding to a final approach axis, and the absolute value differences between the predicted stabilization altitude and the setpoint stabilization altitude.
摘要翻译： 一种方法和装置沿着预定的进场轨迹优化飞行中飞行器的垂直轨迹。 该方法和装置包括使用计算器，其被构造为预测飞机将达到设定点进近速度的预测的稳定高度，作为当前飞行器参数值，理论垂直轨迹和预定的空气动力学模型的函数 飞机的效率。 结构化比较器以确定预测的稳定高度和设定点稳定高度之间的绝对值差异，并将差异与预定高度阈值进行比较。 垂直轨迹确定单元被构造为根据当前飞机参数值，对应于最终进近轴的辅助参数值以及预测的稳定高度和设定点稳定高度之间的绝对值差来确定优化的垂直轨迹。
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2.发明申请公开(公告)号：US20130030611A1
公开(公告)日：2013-01-31
申请号：US13559295
申请日：2012-07-26
申请人： Florian CONSTANS , Mickael Lefebvre
发明人： Florian CONSTANS , Mickael Lefebvre
IPC分类号： G05D1/00
CPC分类号： G08G5/025 , G05D1/0005 , G05D1/0676
摘要： The device (1) includes means (21) for predicting a stabilizing altitude to which the aircraft will reach a setting approach speed, means (22) for comparing predicted stabilizing altitude to a setting stabilizing altitude and means (24) for establishing an optimized vertical trajectory when the difference between predicted stabilizing altitude and setting stabilizing altitude is more than a predetermined altitude threshold.
摘要翻译： 装置（1）包括用于预测飞机将达到设定进近速度的稳定高度的装置（21），用于将预测稳定高度与设定稳定高度进行比较的装置（22）和用于建立优化垂直方向的装置（24） 当预测的稳定高度和设定稳定高度之间的差异大于预定的高度阈值时，轨迹。
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3.发明申请公开(公告)号：US20130030612A1
公开(公告)日：2013-01-31
申请号：US13559325
申请日：2012-07-26
申请人： Florian CONSTANS , Mickael Lefebvre
发明人： Florian CONSTANS , Mickael Lefebvre
IPC分类号： G06F19/00
CPC分类号： G05D1/101 , G01C23/00 , G01C23/005 , G05D1/0005 , G05D1/0077 , G08G5/0013 , G08G5/0021
摘要： Method and device for an optimal management of the energy of an aircraft.The device (1) includes means (5) for determining, in an iterative manner, according to a predicted energy state and according to a management strategy, optimal commands of means (S1,S2, S3, S4, S5, S6) for controlling the energy of the aircraft, which allow the aircraft to reach a given point of a trajectory in a given operational state.
摘要翻译： 用于飞机能量的最佳管理的方法和装置。 装置（1）包括用于根据预测能量状态和根据管理策略以迭代方式确定用于控制的装置（S1，S2，S3，S4，S5，S6）的最佳命令的装置（5） 飞机的能量，使得飞机能够达到给定操作状态下轨迹的给定点。
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4.发明授权公开(公告)号：US08948937B2
公开(公告)日：2015-02-03
申请号：US13559325
申请日：2012-07-26
申请人： Florian Constans , Mickael Lefebvre
发明人： Florian Constans , Mickael Lefebvre
CPC分类号： G05D1/101 , G01C23/00 , G01C23/005 , G05D1/0005 , G05D1/0077 , G08G5/0013 , G08G5/0021
摘要： Method and device for an optimal management of the energy of an aircraft.The device (1) includes means (5) for determining, in an iterative manner, according to a predicted energy state and according to a management strategy, optimal commands of means (S1,S2, S3, S4, S5, S6) for controlling the energy of the aircraft, which allow the aircraft to reach a given point of a trajectory in a given operational state.
摘要翻译： 用于飞机能量的最佳管理的方法和装置。 装置（1）包括用于根据预测能量状态和根据管理策略以迭代方式确定用于控制的装置（S1，S2，S3，S4，S5，S6）的最佳命令的装置（5） 飞机的能量，使得飞机能够达到给定操作状态下轨迹的给定点。
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