2011•Unpublished venueRequires access

Analysis and design of BTT Autopilot with stable yaw rate

Wang Lei, Di Jing-yu, Guo Tao

Abstract

A design and analysis method of BTT Autopilot based on yaw rate stability is proposed. Based on the decoupled model of missile body, three-channels autopilot for a simplified missile model using classical control theory is independently designed, then carry out the 6DOF simulation of system. The results show that the method is appropriate for the coordinated turn control of BTT missile with slow turning rate, and the designed autopilot can follow the instructions quickly, and has a certain ability to resist interference.

About this research paper

What this paper is about

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Key concepts: Autopilot, Missile, Yaw, Control theory (sociology), Computer science, Interference (communication), Missile guidance, Stability (learning theory)