Qualitative analysis of missile guidance problem

Ying Chwan Chiou; Chen-Yuan Kuo

Qualitative analysis of missile guidance problem

Mechanical and Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference 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 language	English (US)
Title of host publication	1997 Guidance, Navigation, and Control Conference
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
Pages	1008-1017
Number of pages	10
State	Published - 1997
Event	Guidance, Navigation, and Control Conference, 1997 - New Orleans, United States Duration: Aug 11 1997 → Aug 13 1997

Other

Other	Guidance, Navigation, and Control Conference, 1997
Country/Territory	United States
City	New Orleans
Period	8/11/97 → 8/13/97

ASJC Scopus subject areas

Control and Systems Engineering
Electrical and Electronic Engineering
Aerospace Engineering

Cite this

@inproceedings{762debf7d9ad49d5b7b11bde68adc190,

title = "Qualitative analysis of missile guidance problem",

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.",

author = "Chiou, {Ying Chwan} and Chen-Yuan Kuo",

year = "1997",

language = "English (US)",

pages = "1008--1017",

booktitle = "1997 Guidance, Navigation, and Control Conference",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

note = "Guidance, Navigation, and Control Conference, 1997 ; Conference date: 11-08-1997 Through 13-08-1997",

}

TY - GEN

T1 - Qualitative analysis of missile guidance problem

AU - Chiou, Ying Chwan

AU - Kuo, Chen-Yuan

PY - 1997

Y1 - 1997

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=84959088254&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84959088254&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84959088254

SP - 1008

EP - 1017

BT - 1997 Guidance, Navigation, and Control Conference

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - Guidance, Navigation, and Control Conference, 1997

Y2 - 11 August 1997 through 13 August 1997

ER -

Qualitative analysis of missile guidance problem

Abstract

Other

ASJC Scopus subject areas

Other files and links

Fingerprint

Cite this