Separation control method, device and equipment for solid binding carrier rocket booster

• Main Author: PENG KUNYA
• Format: Patent
• Language: Chinese; English
• Published: 28.07.2023
• Subjects: AMMUNITION; BLASTING; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; HEATING; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

The invention provides a separation control method, device and equipment for a solid binding carrier rocket booster, which are applied to an on-rocket flight control computer, and the method comprises the steps: generating a core-level engine ignition instruction when detecting that the real-time on-rocket acceleration in the flight process of a rocket is smaller than a preset acceleration threshold value; after the core-level engine ignition instruction is sent out, at least one control instruction is generated according to a preset separation time sequence; and according to the at least one control instruction, the rocket and the solid booster are controlled to be separated and unlocked. According to the scheme provided by the invention, the safety and stability of separation and unlocking of the solid booster and the rocket can be improved. 本发明提供一种固体捆绑运载火箭助推器的分离控制方法、装置及设备，应用于箭上飞控计算机，所述方法包括：在检测到火箭飞行过程中的实时箭上加速度小于预设加速度阈值时，产生芯级发动机点火指令；在所述芯级发动机点火指令发出后，按照预设分离时序，产生至少一个控制指令；根据所述至少一个控制指令，控制所述火箭与固体助推器分离解锁。本发明提供的方案可以