The invention provides a rapid
trajectory planning and guidance method for a
rocket landing section based on flight airspace grid division. The method mainly comprises the steps of establishment of a
rocket landing column coordinate
system, flight airspace grid division, a sequence convex optimization model for solving an absolute
optimal trajectory, online interpolation reduction of the absolute
optimal trajectory, online sequence convex optimization
trajectory optimization and polynomial guidance. The invention aims to solve the problem of high-precision fixed-point landing of a reusable carrier
rocket power landing section, three-dimensional motion of a rocket landing process is decomposed into two-dimensional motion and tangential motion of a
longitudinal plane by using a landing column coordinate
system, the complexity of an optimization model is reduced, an interpolation table is established by using a flight airspace grid division method, and the reliability of the model is improved. According to the method, the absolute
optimal trajectory is rapidly obtained on line, the
global optimization problem is converted into the local
optimization problem, the solving scale of an optimization model is reduced, and the real-time performance of
online optimization is improved while various constraints and fuel optimization are met.