Vibration Control and Structure Integration of antennas on aircraft - Research in NATO SET-131

Conformal and structure integrated antennas mounted on aircraft will play an increasingly important role in future wireless systems. Such antennas have advantages against conventional antenna design but are subject to vibrations and deformations caused e.g. by aerodynamic loads, vehicle motion or mo...

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Published in2013 7th European Conference on Antennas and Propagation pp. 2726 - 2729
Main Authors Knott, P., Loecker, C., Algermissen, S., Sekora, R.
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.04.2013
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ISBN1467321877
9781467321877

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Abstract Conformal and structure integrated antennas mounted on aircraft will play an increasingly important role in future wireless systems. Such antennas have advantages against conventional antenna design but are subject to vibrations and deformations caused e.g. by aerodynamic loads, vehicle motion or moving parts such as the turbine or jet engine. Effects of vibrations and deformations on the performance of radar, navigation or communication systems are in the scope of the NATO research task group SET-131 "Vibration Control and Structure Integration of Antennas". The paper describes research activities within the group and gives an update of a demonstrator system comprising a conformal seven element antenna array with active vibration control.
AbstractList Conformal and structure integrated antennas mounted on aircraft will play an increasingly important role in future wireless systems. Such antennas have advantages against conventional antenna design but are subject to vibrations and deformations caused e.g. by aerodynamic loads, vehicle motion or moving parts such as the turbine or jet engine. Effects of vibrations and deformations on the performance of radar, navigation or communication systems are in the scope of the NATO research task group SET-131 "Vibration Control and Structure Integration of Antennas". The paper describes research activities within the group and gives an update of a demonstrator system comprising a conformal seven element antenna array with active vibration control.
Author Sekora, R.
Knott, P.
Loecker, C.
Algermissen, S.
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  surname: Algermissen
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  email: stephan.algermissen@dlr.de
  organization: Inst. of Composite Struct. & Adaptive Syst., German Aerosp. Centre, Braunschweig, Germany
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  givenname: R.
  surname: Sekora
  fullname: Sekora, R.
  email: robert.sekora@cassidian.com
  organization: EADS Deutschland GmbH Cassidian, Manching, Germany
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Snippet Conformal and structure integrated antennas mounted on aircraft will play an increasingly important role in future wireless systems. Such antennas have...
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SubjectTerms Antenna arrays
Antenna measurements
antennas on aircraft
Arrays
conformal antennas
Radar antennas
structure integrated antennas
vibration control
Vibrations
Title Vibration Control and Structure Integration of antennas on aircraft - Research in NATO SET-131
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