Qualitative analysis of missile guidance problem

Ying Chwan Chiou, Chen-Yuan Kuo

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Based on the possible miss region derived from the kinematics equation of missile-target in two and three dimensional engagements, qualitative analysis is conducted to study capture characteristics of missile guidance commands. From this analysis, sufficient initial condition is assigned which, with the satisfaction of an inequality relation between missile and target commands, can guarantee capture with specific bounds on the line-of-sight rate response. As a special case, true or pure proportional navigation command is derived for straight flight target in two dimensional engagements.

Original languageEnglish (US)
Title of host publication1997 Guidance, Navigation, and Control Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages1008-1017
Number of pages10
StatePublished - 1997
EventGuidance, Navigation, and Control Conference, 1997 - New Orleans, United States
Duration: Aug 11 1997Aug 13 1997

Other

OtherGuidance, Navigation, and Control Conference, 1997
CountryUnited States
CityNew Orleans
Period8/11/978/13/97

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Aerospace Engineering

Fingerprint Dive into the research topics of 'Qualitative analysis of missile guidance problem'. Together they form a unique fingerprint.

  • Cite this

    Chiou, Y. C., & Kuo, C-Y. (1997). Qualitative analysis of missile guidance problem. In 1997 Guidance, Navigation, and Control Conference (pp. 1008-1017). American Institute of Aeronautics and Astronautics Inc, AIAA.