公开(公告)号：US08371535B2

公开(公告)日：2013-02-12

申请号：US12508793

申请日：2009-07-24

Applicant: Michael Grabmeier ,  Christine Stumpp

Inventor： Michael Grabmeier ,  Christine Stumpp

IPC: B64C13/02

CPC classification number: F41F3/0406 ,  B64D1/12 ,  B64D5/00 ,  F41G7/007

Abstract: Unmanned missile and method for releasing the unmanned missile from a carrier aircraft, in which the missile has an autonomous flight control device that acts on control devices of the missile. The method includes adjusting vertical rudders and elevators of the missile into a neutral position in which a respective rudder angle is 0°, separating electrical and mechanical connections between the missile and the carrier aircraft, and detecting, via sensors of the missile, that the separating has occurred. The method also includes activating the autonomous flight control device and automatically controlling the missile with the flight control device and the control devices based upon correction flight condition variables caused by a prevailing downwash between the missile and the carrier aircraft, and automatically controlling the missile with the flight control device and the control devices based on data stored in at least one storage device on the missile.

Abstract translation: 无人驾驶导弹和从载具飞机上释放无人导弹的方法，其中导弹具有作用于导弹的控制装置的自主飞行控制装置。 该方法包括将导弹的垂直方向舵和电梯调整到相应的舵角为0°的中立位置，分离导弹和载具飞机之间的电气和机械连接，以及通过导弹的传感器检测分离 已经发生了。 该方法还包括激活自主飞行控制装置，并根据飞弹控制装置和控制装置自动控制导弹，基于由导弹和载具飞机之间的主流下冲引起的校正飞行情况变量，并自动控制导弹 飞行控制装置和控制装置基于存储在导弹上的至少一个存储装置中的数据。

公开(公告)号：US20120061507A1

公开(公告)日：2012-03-15

申请号：US12508793

申请日：2009-07-24

Applicant: Michael GRABMEIER ,  Christine STUMPP

Inventor： Michael GRABMEIER ,  Christine STUMPP

IPC: F42B15/01 ,  B64D1/12 ,  B64D1/04

CPC classification number: F41F3/0406 ,  B64D1/12 ,  B64D5/00 ,  F41G7/007

Abstract: Unmanned missile and method for releasing the unmanned missile from a carrier aircraft, in which the missile has an autonomous flight control device that acts on control devices of the missile. The method includes adjusting vertical rudders and elevators of the missile into a neutral position in which a respective rudder angle is 0°, separating electrical and mechanical connections between the missile and the carrier aircraft, and detecting, via sensors of the missile, that the separating has occurred. The method also includes activating the autonomous flight control device and automatically controlling the missile with the flight control device and the control devices based upon correction flight condition variables caused by a prevailing downwash between the missile and the carrier aircraft, and automatically controlling the missile with the flight control device and the control devices based on data stored in at least one storage device on the missile.

Abstract translation: 无人驾驶导弹和从载具飞机上释放无人导弹的方法，其中导弹具有作用于导弹的控制装置的自主飞行控制装置。 该方法包括将导弹的垂直方向舵和电梯调整到相应的舵角为0°的中立位置，分离导弹和载具飞机之间的电气和机械连接，以及通过导弹的传感器检测分离 已经发生了。 该方法还包括激活自主飞行控制装置，并根据飞弹控制装置和控制装置自动控制导弹，基于由导弹和载具飞机之间的主流下冲引起的校正飞行情况变量，并自动控制导弹 飞行控制装置和控制装置基于存储在导弹上的至少一个存储装置中的数据。