According to the enterprise research app, recently, Blue Rocket Aerospace Technology Co., Ltd. applied for the publication of a patent for “launch vehicle attitude control method, control device, storage medium and electronic equipment”. According to the patent abstract, the present application provides a launch rocket attitude control method, control device, storage medium, and electronic device. The method includes: based on target attitude angle velocity values of the arrow pitch, yaw, and rolling channel during star arrow separation time obtained offline, off-line design arrow rotation, deceleration time, and attitude angle acceleration of the tilt, yaw, and rolling channels during take-off and deceleration stages, and online real-time calculation of the pitch, yaw, and rolling channels of the star arrow separated in real time. The attitude angular velocity tracking command value; according to The attitude angle velocity tracking command value controls the actual attitude angular velocity of the launch vehicle in real time, keeping the deviation from the pitch, yaw, and rolling channel attitude angle velocity tracking command values within the preset deviation range, thereby stabilizing the flight attitude of the launch vehicle.

According to the enterprise research app, recently, Blue Rocket Aerospace Technology Co., Ltd. applied for the publication of a patent for “launch vehicle attitude control method, control device, storage medium and electronic equipment”. According to the patent abstract, the present application provides a launch rocket attitude control method, control device, storage medium, and electronic device. The method includes: based on target attitude angle velocity values of the arrow pitch, yaw, and rolling channel during star arrow separation time obtained offline, off-line design arrow rotation, deceleration time, and attitude angle acceleration of the tilt, yaw, and rolling channels during take-off and deceleration stages, and online real-time calculation of the pitch, yaw, and rolling channels of the star arrow separated in real time. The attitude angular velocity tracking command value; according to The attitude angle velocity tracking command value controls the actual attitude angular velocity of the launch vehicle in real time, keeping the deviation from the pitch, yaw, and rolling channel attitude angle velocity tracking command values within the preset deviation range, thereby stabilizing the flight attitude of the launch vehicle.