The server is under maintenance between 08:00 to 12:00 (GMT+08:00), and please visit later.
We apologize for any inconvenience caused
Login  | Sign Up  |  Oriprobe Inc. Feed
China/Asia On Demand
Journal Articles
Bookmark and Share
Calculating and Research of Initial Value of Quaternion of Strapdown Inertial Guidance in Missile’s Mobile Launching
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.
Related Articles
No related articles found