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Calculating and Research of Initial Value of Quaternion of Strapdown Inertial Guidance in Missile’s Mobile Launching
Author(s): 
Pages: 28-33
Year: Issue:  4
Journal: Aerospace Control

Keyword:  Strapdown inertial guidance\ \+*Quaternion\ Coordinate-gyration;
Abstract: This paper derives three methods of calculating initial value of quaternion of strap-down inertial control and guide homing in missile’s mobile launching. At first how to represent the rotating reference frame by the method of quaternion is introduced and then two methods of representing reference frame rotating continuously are explored, in the end, merits and demerits of the three methods have been comprised.
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