Advances in Aerospace Guidance, Navigation and Control: by Sven Lorenz, Florian M. Adolf (auth.), Florian Holzapfel,

By Sven Lorenz, Florian M. Adolf (auth.), Florian Holzapfel, Stephan Theil (eds.)

Over the previous couple of many years, either the aeronautics and house disciplines have vastly encouraged advances in controls, sensors, info fusion and navigation. lots of these achievements that made the note “aerospace” synonymous with “high–tech” have been enabled through options in advice, navigation and control.

Europe has obvious a powerful trans-national consolidation technique in aerospace over the past few many years. many of the noticeable items, like advertisement plane, warring parties, helicopters, satellites, launchers or missiles, are usually not made via a unmarried kingdom – they're the culmination of cooperation. No eu state on its own hosts a really expert assistance, navigation and controls group sufficiently big to hide the entire spectrum of disciplines. in spite of the fact that, on a ecu scale, mutual trade of principles, thoughts and recommendations is enriching for all. the first CEAS expert convention on information, Navigation and keep watch over is an try and convey this group together.

This publication is a variety of papers awarded on the convention. All submitted papers have undergone a proper assessment method in compliance with stable magazine practices. the simplest papers were steered by means of the reviewers to be released during this book.

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Additional resources for Advances in Aerospace Guidance, Navigation and Control: Selected Papers of the 1st CEAS Specialist Conference on Guidance, Navigation and Control

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Html 5. org/ 6. I. com 7. : Synthesis and validation of flight control for UAV. D. thesis, University of Minnesota (2009) 8. Matlab, Simulink, Real-Time Windows Target 3 User’s Guide. The MathWorks Inc. (2008) 9. org/ 10. htm 11. : Development of a low-cost sub-scale aircraft for flight research: The FASER project. In: 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference (2006-3306) 12. : Wind tunnel database development using modern experiment design and multivariate orthogonal functions.

E. coupled, nonlinear vehicle. The control design objectives are to track the reference angles of attack, sideslip and bank in the face of the established noise and uncertain levels with desired deviations of less than 2 degrees, and with acceptable short-term deviations of less than 4 degrees. A. Longitudinal Motion Controller Design The design rationale for the longitudinal motion is that of angle-of-attack tracking through an ideal-model formulation. The same design rationale and plant set-up as for the baseline control design are used [19].

Researchers at the NASA Langley Research Center performed significant static wind tunnel tests of an Ultra Stick 120 as part of the FASER development effort [11, 12]. This data is being implemented into the UAV simulation and will be openly available for research, education, and collaboration. This data set includes control surface and thrust effects over an angle of attack range of -5 to 40 degrees and an angle of sideslip range of +/- 30 degrees. As mentioned previously, the UAV Research Group operates an Ultra Stick 120 that was donated by NASA LaRC.

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