Robust Gyro-free Attitude Estimation for a Small Fixed-wing Unmanned Aerial Vehicle
Author:
Affiliation:
1. School of Engineering and Information Technology; University of New South Wales at the Australian Defence Force Academy; Canberra; ACT; 2600; Australia
Publisher
Wiley
Subject
Control and Systems Engineering
Reference24 articles.
1. Single antenna GPS-based aircraft attitude determination;Kornfeld;J. Inst. Navigation,1998
2. Mini-UAV attitude estimation using an inertially stabilized payload;Oshman;IEEE Trans. Aerosp. Electron. Syst.,1999
3. Applications of global positioning system velocity-based attitude information;Kornfeld;AIAA J. Guid., Control Dyn.,2001
4. System identification modelling of a small-scale unmanned rotorcraft for flight control design;Mettler;J. Am. Helicopter Soc.,2002
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