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公开(公告)号：US08285425B2
公开(公告)日：2012-10-09
申请号：US11629148
申请日：2005-06-06
申请人： Maria Jesús Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martínez , Francisco José Ibañez Colás , Andrés Herrera Martín
发明人： Maria Jesús Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martínez , Francisco José Ibañez Colás , Andrés Herrera Martín
CPC分类号： G05D1/101
摘要： The invention relates to an unmanned air vehicle control system and method, designed such that, in one mission mode, the vehicle follows the mission route. The system comprises means (400, 450) for storing data indicating at least one auxiliary route (4000, 4001, 4002, 4003), such that each of a plurality of the mission route segments (10, 20), is assigned at least part (30, 31, 32, 33) of at least one auxiliary route. Furthermore, the system comprises route change means (53) designed for, as a response to a mission abandonment event (52), determining which part of which auxiliary route is assigned to the mission route segment where the vehicle is located, such that the vehicle can change the mission route to the corresponding auxiliary route.
摘要翻译： 本发明涉及一种无人驾驶飞行器控制系统和方法，其设计使得在一个任务模式中，车辆遵循任务路线。 该系统包括用于存储指示至少一个辅助路线（4000,4001,4002,4003）的数据的装置（400,450），使得多个任务路线段（10,20）中的每一个被分配至少部分 （30,31,32,33）的至少一个辅助路线。 此外，系统包括设计用于作为对任务放弃事件（52）的响应的路线改变装置（53），确定哪个辅助路线的哪一部分被分配给车辆所在的任务路线段，使得车辆 可以将任务路线改为相应的辅助路线。
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2.发明授权Method for controlling control parameters in an air vehicle and system of controlling an air vehicle 失效用于控制空中车辆中的控制参数的方法和控制飞行器的系统公开(公告)号：US07706932B2
公开(公告)日：2010-04-27
申请号：US11606412
申请日：2006-11-30
申请人： Maria Jesus Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martinez , Francisco José Ibañez Colás , Andrés Herrera Martin
发明人： Maria Jesus Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martinez , Francisco José Ibañez Colás , Andrés Herrera Martin
IPC分类号： G05D1/08
CPC分类号： G05D1/101
摘要： According to the method of the invention, control parameters V indicating speed, R indicating turn characteristics and γ indicating a path angle are determined such that these parameters are maintained between limits, and such that one of them deviates as little as possible from a corresponding control input parameter Ri. In order to maintain (as much as possible) the value of R unchanged, V can be varied. The method may include the calculation of the maximum and minimum thrust available.
摘要翻译： 根据本发明的方法，确定指示速度的控制参数V，指示转弯特性的R和指示路径角的γ，使得这些参数保持在极限之间，并且使得它们之一尽可能少地偏离相应的控制 输入参数Ri。 为了维持（尽可能多），R的值不变，V可以变化。 该方法可以包括可用的最大和最小推力的计算。
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3.发明申请Method for controlling control parameters in an air vehicle and system of controlling an air vehicle 失效用于控制空中车辆中的控制参数的方法和控制飞行器的系统公开(公告)号：US20080133069A1
公开(公告)日：2008-06-05
申请号：US11606412
申请日：2006-11-30
申请人： Maria Jesus Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martinez , Francisco Jose Ibanez Colas , Andres Herrera Martin
发明人： Maria Jesus Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martinez , Francisco Jose Ibanez Colas , Andres Herrera Martin
IPC分类号： G06F17/00
CPC分类号： G05D1/101
摘要： According to the method of the invention, control parameters V indicating speed, R indicating turn characteristics and γ indicating a path angle are determined such that these parameters are maintained between limits, and such that one of them deviates as little as possible from a corresponding control input parameter Ri. In order to maintain (as much as possible) the value of R unchanged, V can be varied. The method may include the calculation of the maximum and minimum thrust available.
摘要翻译： 根据本发明的方法，确定指示速度的控制参数V，指示转弯特性的R和指示路径角的伽马，使得这些参数保持在极限之间，并且使得它们之一尽可能少地偏离相应的控制 输入参数Ri。 为了维持（尽可能多），R的值不变，V可以变化。 该方法可以包括可用的最大和最小推力的计算。
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公开(公告)号：US20080243317A1
公开(公告)日：2008-10-02
申请号：US11629148
申请日：2005-06-06
申请人： Maria Jesus Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martinez , Francisco Jose Ibanez Colas , Andres Herrera Martin
发明人： Maria Jesus Morales De La Rica , Sergio De La Parra Carque , Francisco Javier Angel Martinez , Francisco Jose Ibanez Colas , Andres Herrera Martin
CPC分类号： G05D1/101
摘要： The invention relates to an unmanned air vehicle control system and method, designed such that, in one mission mode, the vehicle follows the mission route. The system comprises means (400, 450) for storing data indicating at least one auxiliary route (4000, 4001, 4002, 4003), such that each of a plurality of the mission route segments (10, 20), is assigned at least part (30, 31, 32, 33) of at least one auxiliary route. Furthermore, the system comprises route change means (53) designed for, as a response to a mission abandonment event (52), determining which part of which auxiliary route is assigned to the mission route segment where the vehicle is located, such that the vehicle can change the mission route to the corresponding auxiliary route.
摘要翻译： 本发明涉及一种无人驾驶飞行器控制系统和方法，其设计使得在一个任务模式中，车辆遵循任务路线。 该系统包括用于存储指示至少一个辅助路线（4000,4001,4002,4003）的数据的装置（400,450），使得多个任务路线段（10,20）中的每一个被分配至少部分 （30,31,32,33）的至少一个辅助路线。 此外，系统包括设计用于作为对任务放弃事件（52）的响应的路线改变装置（53），确定哪个辅助路线的哪一部分被分配给车辆所在的任务路线段，使得车辆 可以将任务路线改为相应的辅助路线。
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