ScholarLens Back to search
2001•Tactical Missile TechnologyRequires access

Applicability Analysis of Structure of Autopilot and Static-unstable Missile Body

Dai Liu

Open publisher page 1 citations

Abstract

The active control technology(ACT)had been used in design of air to air missile more and more.How to control the unstable missile body seems to be very important.The characteristic and applicability to the unstable missile body of six kind of autopilot were analysed. The result of research discovered that acceleration feedback three loops autopilot seems to be effective for the control of unstable missile body.

About this research paper

What this paper is about

The active control technology(ACT)had been used in design of air to air missile more and more.How to control the unstable missile body seems to be very important.The characteristic and applicability to the unstable missile body of six kind of autopilot were analysed. The result of research discovered that acceleration feedback three loops autopilot seems to be effective for the control of unstable missile body.

Why it matters

OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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

The active control technology(ACT)had been used in design of air to air missile more and more.How to control the unstable missile body seems to be very important.The characteristic and applicability to the unstable missile body of six kind of autopilot were analysed. The result of research discovered that acceleration feedback three loops autopilot seems to be effective for the control of unstable missile body.

Key concepts: Autopilot, Missile, Acceleration, Engineering, Control theory (sociology), Air-to-air missile, Missile guidance, Aerospace engineering

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Applicability Analysis of Structure of Autopilot and Static-unstable Missile Body — Research Paper | ScholarLens