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THE ENGINEERING DESIGN PROBLEM OF STRAPDOWN SYSTEM IN VERTICAL LAUNCH TACTICAL MISSILE
Author(s): 
Pages: 37-43
Year: Issue:  4
Journal: Aerospace Control

Keyword:  Tactical missileVertical launchingStrapdown inertial guidanceGuidonce control;
Abstract: The engineering application problem of strapdown inertial navigation system in ver-tical launch tactical missile is discussed intensively in this paper. The problem includes how touse missile attitude information, how to determine calculation errors, what initial alignmentmethod will be used and how to describe dynamic characteristics etc.
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