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43

Selected Highlights 2017

Institute of Lightweight Structures

Flaps and movable devices of aircraft show gaps and

discontinuities, which result in additional drag and noise

among other effects. The design, manufacturing and

testing of flexible, shape-adaptive structures were at the

center of research at the Institute for Lightweight Struc-

tures, to close the gaps and increase the overall efficiency

of such systems.

Institute of Flight System Dynamics together with

TUM-IAS Focus Group ‘Aircraft Stability and Control’:

One key challenge for UAV is to ensure a safe flight, as

there is no pilot on board who could react to unexpected

behavior due to system failures, external disturbances

(turbulence, gusts) or model errors. Therefore, the Institute

of Flight System Dynamics together with the TUM-IAS

Focus Group ‘Aircraft Stability and Control’ developed an

innovative autoflight system (AFS) for SAGITTA which ena-

bles fully automatic flight missions from take-off to stand-

still after landing. Since the novel aircraft configuration

had never been flown before, it was a major design driver

for the AFS to cope with the widest possible spectrum of

model uncertainties. The researchers were rewarded with

extremely successful flight tests. Both flights of SAGITTA

could be accomplished fully automatically and demon-

strated excellent flying characteristics.

Besides the successful flight campaign a large amount of

expertise as well as conference publications and journal

articles have been provided to the public domain. With the

return of the demonstrator to Germany, the researchers

are eager to extract more valuable data from the success-

ful flights to further proceed in the research on UAVs.

Univ.-Prof. Dr.-Ing. Mirko Hornung

Aircraft Design

www.lls.mw.tum.de sekretariat@lls.mw.tum.de

Phone +49.89.289.15981

Contact