发明名称 Stationary and Mobile Test Device for Missiles
摘要 A stationary test device for a missile includes a retaining device for an avionics testpiece of the missile, where the retaining device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a display device configured to display information on the missile surroundings, where the display device is configured to be moved inside a virtual plane by a translational carriage system. The display device can be detected by the avionics testpiece if the avionics testpiece is disposed on the retaining device. A mobile test device for the missile includes a flight platform, a carrier device mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a control module, where the control module is configured to control the flight platform for taking off on a specified reference trajectory, control the carrier device for orientation of the avionics testpiece, and store navigation data generated by the avionics testpiece. Finally, a test system for the missile includes the stationary test device and the mobile test device.
申请公布号 US2016252328(A1) 申请公布日期 2016.09.01
申请号 US201615048202 申请日期 2016.02.19
申请人 MBDA Deutschland GmbH 发明人 LIMMER Michael;GALLHAUSER Thomas;SURAUER Michael Alois;SURAUER Christian;GEIDEK Franz
分类号 F41G7/00;G06F17/50;B64C27/08 主分类号 F41G7/00
代理机构 代理人
主权项 1. A mobile test device for a missile, comprising a flight platform; a carrier device mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier device enables a movement of the avionics testpiece in three rotational degrees of freedom; and a control module configured to: control the flight platform for taking off on a specified reference trajectory, control the carrier device for orientation of the avionics testpiece, and store navigation data generated by the avionics testpiece.
地址 Schrobenhausen DE