A robust midcourse guidance law based on the zero effort miss is designed for the middle flying stage of exo-atmospheric intercept with the fuel-exhaustion-shutoff solid engine.

It has designed a software pack for the analysis of midcourse guidance s precision,which includes the initial alignment module and other several modules.

The calculation method of mid-course guidance error of missile and the simulation method of target acquisition probability are described in detail.

Towards the gaining altitude segment in the mid-course guidance of the ship-to-air missile beyond visual range,the procedure circinal arcs were applied to design the trajectory and the altitude and the pitch angle instructions were obtained.

After bringing forward the accuracy demands of the mid-course guidance for missile attacking ground on the Beidou position system,this paper analyses the effects of altitude error on the position accuracy in detail.

Midcourse phase of long and medium range air-to-air missiles usually adopt compound guidance-inertial navigation system + command guidance system.

Application of Tianhewang Integrated Navigation System to Middle Guidance of Gruise Missile;

Base on one cruise missile,this paper analyzes the factors to influence the middle guidance precision of cruise missile,and makes simulation.

Variable Structure Midcourse Guidance Law with Angle Constraint for Anti-Ship Missile;

A Optimal Midcourse Guidance Law Using Neural Network;

Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile;