Existing design methods for the stable loop of missile are, to our best knowledge, rather complicated.

Discrete variable structure control of digital stabilization loop for inertial platform;

Design on stabilization loop of roll-isolated SINS in spinning projectile

Based on the airborne EO system principle analysis,the stabilization control loop of the system is modelled and a stabilization loop configuration is proposed.

Study on adaptive stabilizing circuit of INS;

This paper discusses the design problem of active disturbance rejection control (ADRC) for the inertial platform stabilizing circuits.

And the stabilizing circuits are one of the most important parts in INS, which eliminate the disturbance and make the platform to follow the local level coordinate.

Multi-loop control of inertial platform servo loop;

The stabilizing loop is the base of the high-precision tracking and the design of stabilizing loop affects the whole tracking system’s performance directly.

To investigate active disturbance rejection control(ADRC) of the stabilizing loop for roll-isolated laser gyro strap-down inertial navigation system(RLGSINS) which is available to spinning vehicles,the approach called ADRC is adopted extensively.

It has been concluded that the inner loop of a three-loop autopilot is an attitude autopilot,it can make an unstable missile stable;missile aerodynamic coefficient change and fin control surface bias do not have effects on the steady state outputs of three-loop autopilots.