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

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

Over the previous few many years, either the aeronautics and house disciplines have enormously encouraged advances in controls, sensors, facts fusion and navigation. a lot of these achievements that made the notice “aerospace” synonymous with “high–tech” have been enabled by means of options in advice, navigation and control.

Europe has obvious a powerful trans-national consolidation strategy in aerospace during the last few a long time. lots of the noticeable items, like advertisement airplane, combatants, helicopters, satellites, launchers or missiles, will not be made through a unmarried kingdom – they're the end result of cooperation. No eu kingdom on its own hosts a really good counsel, navigation and controls neighborhood big enough to hide the complete spectrum of disciplines. in spite of the fact that, on a ecu scale, mutual trade of rules, recommendations and options is enriching for all. the first CEAS expert convention on assistance, Navigation and keep watch over is an try and carry this group together.

This ebook is a variety of papers provided on the convention. All submitted papers have undergone a proper evaluate strategy in compliance with reliable magazine practices. the simplest papers were steered by means of the reviewers to be released during this book.

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Extra 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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Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air. NASA Technical Memorandum 209357 (September 1999) 6. : HL20 aeroblockset MATLAB. The Mathworks 7. : Six-Degree-of-Freedom Guidance and Control-Entry Analysis of the HL-20. Journal of Spacecraft and Rockets 30(5) (1993) 8. : Design examples using mu-synthesis: Space shuttle lateral axis FCS during re-entry. In: IEEE Control Decision Conference, vol. 25, pp. 2218–2223 (1986) 9. : Application of LPV modeling, design and analysis methods to a re-entry vehicle.

In: AIAA GNC 2009 (2009) 13. : Nonlinear WorstCase Analysis of an LPV Controller for Approach-Phase of a Re-entry Vehicle. In: AIAA GNC 2009 (2009) 14. : Analysis of the Controlled NASA HL20 Atmospheric Re-entry Vehicle based on Dynamic IQCs. In: AIAA GNC 2009 (2009) 15. : IQC-Based IQC LPV Controller Synthesis for the NASA HL20 Atmospheric Re-entry Vehicle. In: AIAA GNC 2009 (2009) A Linear Parameter Varying Controller for a Re-entry Vehicle Benchmark 27 16. : Research on Gain Scheduling. Automatica 36, 1401–1425 (2000) 17.

The key concept of the two step method, is that the identification procedure has been split into two consecutive steps, as substantiated in ref. [9]. More precisely, the global non-linear one step identification method is decomposed in two separate steps, where the nonlinear part is isolated in the aircraft state estimation step. Consequently, the aerodynamic model parameter identification procedure in the second step can be simplified to a procedure which is linear in the parameters, but involves nonlinear regressors.

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