AGILE MISSILE DYNAMICS AND CONTROL

Authors
Citation
Ka. Wise et Dj. Broy, AGILE MISSILE DYNAMICS AND CONTROL, Journal of guidance, control, and dynamics, 21(3), 1998, pp. 441-449
Citations number
8
Categorie Soggetti
Instument & Instrumentation","Aerospace Engineering & Tecnology
ISSN journal
07315090
Volume
21
Issue
3
Year of publication
1998
Pages
441 - 449
Database
ISI
SICI code
0731-5090(1998)21:3<441:AMDAC>2.0.ZU;2-Z
Abstract
The dynamics and technical challenges of controlling missiles capable of high-angle-of-attack Eight are discussed. The missile control effec ters discussed include thrust vectoring, reaction jet thrusters, and a erodynamic tail surfaces. A control power analysis is summarized that indicates the effectiveness of these control effecters over the missil e's flight envelope. The six-degree-of-freedom dynamics for high-angle -of-attach missile Eight control are presented. Autopilot design model s and nonlinear simulation results demonstrating high angle-of-attack flight are also presented.