Recent advances in low cost sensor technologies and nonlinear estimation techniques are applicable to the navigation of gun-launched projectiles. A method for attitude (i.e. angular orientation) estimation is presented that uses magnetometers aided by angular rate sensors. Nonlinear state estimators provide the filtering mechanisms to combine the measurements based on their levels of accuracy. Results are presented using the extended Kalman filter (EKF) and the unscented Kalman filter (UKF), and the UFK is shown to outperform the EKF. The proposed method is demonstrated to provide a full attitude solution while satisfying the stringent requirements of gun-launched projectiles.
29.1 NAVIGATION OF PROJECTILE AND SPECIFIC FEATURES 29.1.1 STATE OF THE ART FOR ATTITUDE ESTIMATION Guided ... its embedded system needs to know in real time its angular position (attitude), velocity, and ideally its position.
The fifth International conference on Nonlinear Problems in Aviation and Aerospace was held at University of Timlsoara, Romania in June 2004. This proceedings publication includes keynote addresses, invited lectures and...
This book intends to provide the reader with both a generic and comprehensive view of contemporary data fusion methodologies for attitude estimation, as well as the most recent researches and novel advances on multisensor attitude ...
. The book is well organized ... . The discussion in the book ... should be accessible to readers with some elementary understanding of aerodynamic principles. For the expert, the book is full of open problems ... . Its scope is extensive .
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