A Design Method of Missile Acceleration Autopilot Based on Active Disturbance Rejection Control
نویسندگان
چکیده
منابع مشابه
Systematic Gain-scheduling Control Design: a Missile Autopilot Example
The missile autopilot was designed using linear parameter-varying (LPV) control techniques. The controller provides exponential stability guarantee and performance bound in terms of induced L2 norm for the missile plant. The systematic gain-scheduling approach is motivated by the recent development in LPV control theory and provides a well founded and systematic procedure for high performance m...
متن کاملA Novel Motion Control Design Approach Based On Active Disturbance Rejection
A new digital control solution to motion control problems is proposed. It is based on a unique active disturbance rejection concept, where the disturbances are estimated using an extended state observer (ESO) and compensated in each sampling period. The dynamic compensation reduces the motion system to approximately a double integrator which can be easily controlled using a nonlinear proportion...
متن کاملVoltage Control of Three Phase Inverters by Using Active Disturbance Rejection Control
Control of three phase inverters has been an important issue in recent years. This paper proposes active disturbance rejection control (ADRC) scheme for controlling three phase inverters. The main advantage of ADRC that motivated us for using this controller for inverter is that it is model independent. This controller is used in a double loop structure including an inner current loop and oute...
متن کاملMissile Autopilot Design for Agile Turn Control During Boost-Phase
This paper presents the air-to-air missile autopilot design for a 180° heading reversal maneuver during boost-phase. The missile’s dynamics are linearized at a set of operating points for which angle of attack controllers are designed to cover an extended flight envelope. Then, angle of attack controllers are designed for this set of points, utilizing a pole-placement approach. The controllers’...
متن کاملMissile Longitudinal Autopilot Design Using A New Suboptimal Nonlinear Control Method
In this paper, a missile longitudinal autopilot is designed using a new nonlinear control synthesis technique (called theθ -D approximation). The particular D θ − methodology used in this paper is referred to as the D θ − 2 H design. The D θ − technique can achieve suboptimal solutions to a class of nonlinear optimal control problems in the sense that it solves the Hamilton-Jacobi-Bellman (HJB)...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: IOP Conference Series: Materials Science and Engineering
سال: 2020
ISSN: 1757-899X
DOI: 10.1088/1757-899x/768/4/042011