The Design and Simulation of Three Dimensional Self Calibration Guidance Law

CHEN  Shengqi; ZHOU  Jun

doi:10.15892/j.cnki.djzdxb.2011.06.033

Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 6: 1 - 4

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.06.033

MISSILES AND GUIDANCE TECHNOLOGY

The Design and Simulation of Three Dimensional Self Calibration Guidance Law

CHEN Shengqi ,
ZHOU Jun

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Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2011-03-06

Online published: 2025-05-30

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Abstract

In this paper, a kind of three-dimensional guidance law for the air-to-surface attacking mode was derived based on the variable structure control (VSC) theory, then the relationship between the measurement error and guidance error was investigated and discussed thoroughly, the 3-D guidance law based on VSC was modified for easy implementation, the performance of modified guidance law was validated through the comparison between traditional guidance law and modified guidance law based on the computer simulation.

Key words： measurement error; guidance error; 3-D guidance law; variable structure control

Cite this article

CHEN Shengqi , ZHOU Jun . The Design and Simulation of Three Dimensional Self Calibration Guidance Law[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(6) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2011.06.033

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