By Sven Lorenz, Florian M. Adolf (auth.), Florian Holzapfel, Stephan Theil (eds.)
Over the previous few a long time, either the aeronautics and area disciplines have significantly motivated advances in controls, sensors, info fusion and navigation. a lot of these achievements that made the notice “aerospace” synonymous with “high–tech” have been enabled through strategies in counsel, navigation and control.
Europe has noticeable a robust trans-national consolidation technique in aerospace during the last few many years. many of the noticeable items, like advertisement plane, opponents, helicopters, satellites, launchers or missiles, aren't made via a unmarried kingdom – they're the culmination of cooperation. No eu kingdom on its own hosts a really expert assistance, navigation and controls group big enough to hide the total spectrum of disciplines. notwithstanding, on a ecu scale, mutual trade of rules, strategies and options is enriching for all. the first CEAS expert convention on suggestions, Navigation and regulate is an try and deliver this group together.
This publication is a variety of papers offered on the convention. All submitted papers have undergone a proper assessment approach in compliance with stable magazine practices. the simplest papers were urged by means of the reviewers to be released during this book.
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Additional info for Advances in Aerospace Guidance, Navigation and Control: Selected Papers of the 1st CEAS Specialist Conference on Guidance, Navigation and Control
And actually, the current software tools used to synthesize the LPV controller directly takes the weights and interconnection used in the standard LTI H∞ design set-up and facilitates its tuning to arrive at the desired global performance. Indeed, the synthesis of design-point LTI H∞ controllers can be seen as a first step in the application of this LPV technique. LTI H∞ optimization is a design technique where specification of performance and robustness objectives is the main driver in correctly posing the mathematical optimization problem –as opposed to other control synthesis techniques where satisfaction of the objectives is evaluated after the design.
The LPV technique used is the A Linear Parameter Varying Controller for a Re-entry Vehicle Benchmark 19 so-called Single Quadratic Lyapunov Function (SQLF) approach . Essentially, this technique synthesizes a LPV controller by means of finding a single quadratic Lyapunov function, not depending on the varying parameter vector, that satisfies an LPV version of the well-known bounded real lemma (BRL). In practice, it searches for a Lyapunov function valid for a set of linear matrix inequalities (LMIs) corresponding to the satisfaction of the BRL at a grid of values of the varying parameter vector that defines the LPV plant.
55kg of payload. The Mini Ultra Stick is an approximately 50% scale model of the Ultra Stick 120, with the same basic configuration. The UAV Research Group currently uses this aircraft as a wind tunnel model, as the smaller size enable it to fit into the AEM department’s low speed wind tunnel. The specifications of the three Ultra Stick aircraft are given in Table 1. The Ultra Stick aircraft family is marketed as a trainer-level aerobatic aircraft, so it is relatively easy for a moderately skilled R/C pilot to fly, but is still capable of highly dynamic manuevering flight.