The invention provides a target drone launching control method and device, a target drone flight control computer and a storage medium and belongs to the field of target drone control. The method comprises steps of detecting a pitch angle of a target drone in response to a received drone transmitting instruction; determining whether the target drone is in a launch state or a non-launch state according to the pitch angle and a preset angle range of a launch window; and if the target drone is in the launching state, sending an ignition instruction to the ignition controller, wherein the ignitioninstruction is used for controlling the rocket to ignite to launch the target drone. The method is advantaged in that whether a pitch angle is within a preset angle range of a launching window or notis judged by detecting a pitch angle of a target drone aircraft, so a target drone aircraft is launched when the target drone aircraft is in a launching state, and accuracy of a launching angle of the target drone aircraft is improved.
本发明提供一种靶机发射控制方法、装置、靶机飞控计算机及存储介质,属于靶机控制领域。该方法包括:响应接收到的靶机发射指令,检测目标靶机的俯仰角;根据俯仰角以及预设的发射窗口的角度范围,确定目标靶机为发射状态,还是不可发射状态;若目标靶机为发射状态,则向点火控制器发送点火指令,点火指令用于控制火箭点火以发射目标靶机。通过检测目标靶机的俯仰角判断该俯仰角是否在预设的发射窗口的角度范围,以实现靶机在发射状态时,发射目标靶机,提高了靶机发射角度的准确率。
Target drone launching control method and device, target drone flight control computer and storage medium
靶机发射控制方法、装置、靶机飞控计算机及存储介质
2020-09-08
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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