Guidance Control of a Missile With Noisy Inertial Sensors

By Ali Galip YILDIRIM

This thesis work deals with the design of a guidance control architecture using sliding mode control for a missile equipped with an inertial navigation system, gyroscopes and accelerometers. The... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 3639243226
• ISBN13: 9783639243222
• Release Date: March 2010
• Publisher: VDM Verlag
• Length: 176 Pages
• Weight: 0.59 lbs.
• Dimensions: 0.4" x 6.0" x 9.0"