P
Peter Vörsmann
Researcher at Braunschweig University of Technology
Publications - 71
Citations - 793
Peter Vörsmann is an academic researcher from Braunschweig University of Technology. The author has contributed to research in topics: Space debris & Debris. The author has an hindex of 11, co-authored 71 publications receiving 721 citations.
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Measuring the Wind Vector Using the Autonomous Mini Aerial Vehicle M2AV
TL;DR: In this paper, a meteorological mini unmanned aerial vehicle (M2AV) was used for measuring the meteorological wind, which is the vector difference between the aircraft speed relative to the earth (inertial velocity) and the airflow (true airspeed) computed from five-hole-probe pressure measurements in combination with calibration coefficients obtained during wind tunnel calibration.
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First application of the meteorological Mini-UAV 'M2AV'
TL;DR: In this article, the Meteorological Mini-UAV (M 2 AV) is used to perform turbulence and wind vector measurements within the atmospheric boundary layer and permits very short measurement cycles as an economic supplement during meteorological campaigns.
Journal ArticleDOI
Active debris removal of multiple priority targets
Vitali Braun,A. Lüpken,S. Flegel,Johannes Gelhaus,Marek Möckel,Christopher Kebschull,Carsten Wiedemann,Peter Vörsmann +7 more
TL;DR: In this paper, chemical and electric propulsion systems were analysed with the main focus on removing multiple targets within one single mission, chosen from a previously defined priority list in order to enhance the mission efficiency.
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2012 Special Issue: Fault-tolerant nonlinear adaptive flight control using sliding mode online learning
TL;DR: An expanded nonlinear model inversion flight control strategy using sliding mode online learning for neural networks is presented, which treats the neural network as a controlled system and allows a stable, dynamic calculation of the learning rates.
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Development of in-situ Space Debris Detector
TL;DR: In this article, an innovative detection concept is proposed that utilises existing spacecraft components for detection purposes, and an estimate of the expected sensitivity of the proposed detector concept as well as examples for its implementation into large and small spacecraft are presented.