Spinning rotation rocket self guidance method having front imaging nose section decoupled spinning body and transmission mechanism nose/main body image transmitting

摘要

The spinning rotation rocket has a front nose section (2) and a body (1). There is an imaging unit (10) and trajectory correction unit (11). The nose and body sections are decoupled in rotation. A mechanism (5) creates a differential spin between the two sections. A transmission mechanism (17) transmits the image from the nose to the main body.