Feasibility Study of Attitude Determination for All-Rotating Unmanned Aerial Vehicles in Steady Flight

Author:

Matič Gašper,Jankovec Marko,Jurman David,Topič Marko

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Artificial Intelligence,Industrial and Manufacturing Engineering,Mechanical Engineering,Control and Systems Engineering,Software

Reference40 articles.

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2. Beer, F.P., Johnston, E.R.J., Mazurek, D.F., Cornwell, P.J., Eisenberg, E.R.: Vector Mechanics for Engineers: Statics and Dynamics, 9th edn, chap. 9. McGraw-Hill, Boston (2010)

3. Bekkeng, J.K.: Prototype Development of a Low-Cost Sounding Rocket Attitude Determination System and an Electric field Instrument. Phd thesis, University of Oslo, Oslo, Norway (2007). http://tid.uio.no/~jankbe/Filer/PhD_JKB_200207.pdf

4. Bonnet, S., Bassompierre, C., Godin, C., Lesecq, S., Barraud, A.: Calibration methods for inertial and magnetic sensors. Sensors Actuators A Phys. 156 (2), 302–311 (2009). doi: 10.1016/j.sna.2009.10.008 . http://linkinghub.elsevier.com/retrieve/pii/S0924424709004324

5. Brown, T.G.: Harsh military environments and microelectromechanical (MEMS) devices. In: Sensors, 2003. Proceedings of IEEE, vol. 2, pp. 753–760. IEEE (2003), doi: 10.1109/ICSENS.2003.1279042

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