2007Microcomputer InformationRequires access

Design of the dynamic analyse system for missile pilot stabilized loop

Su An

Open publisher page 0 citations

Abstract

For researching parameters of missile stabilized loop to performance effect of missile control system,a dynamic analyse sys-tem for missile pilot stabilized loop is devised. The system uses a industrial control computer as a core,the A/D、D/A、and time arithmometer boards are assembled as a cascade structure. Using automatic test hardware facility and increasing software and hardware anti-jamming measures,it improves test precision. Test result indicates that the system can be applied well in the test parameter analyse of the pilot stabilized loop,and has good theory value and practical significance.

About this research paper

What this paper is about

For researching parameters of missile stabilized loop to performance effect of missile control system,a dynamic analyse sys-tem for missile pilot stabilized loop is devised. The system uses a industrial control computer as a core,the A/D、D/A、and time arithmometer boards are assembled as a cascade structure. Using automatic test hardware facility and increasing software and hardware anti-jamming measures,it improves test precision. Test result indicates that the system can be applied well in the test parameter analyse of the pilot stabilized loop,and has good theory value and practical significance.

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

For researching parameters of missile stabilized loop to performance effect of missile control system,a dynamic analyse sys-tem for missile pilot stabilized loop is devised. The system uses a industrial control computer as a core,the A/D、D/A、and time arithmometer boards are assembled as a cascade structure. Using automatic test hardware facility and increasing software and hardware anti-jamming measures,it improves test precision. Test result indicates that the system can be applied well in the test parameter analyse of the pilot stabilized loop,and has good theory value and practical significance.

Key concepts: Missile, Computer science, Hardware-in-the-loop simulation, Cascade, Loop (graph theory), Software, Simulation, Missile guidance

Related papers

Back to paper searchBrowse research topicsOriginal source
Design of the dynamic analyse system for missile pilot stabilized loop — Research Paper | ScholarLens