Publications

M. Hirth, N. Brandt, and W. Fichter. Inertial Sensing for Future Gravity Missions. GEOTECHNOLOGIEN Science Report, Observation of the System Earth from Space, 17Rheinische Friedrich-Wilhelms-Universität, Bonn, 2010. [PUMA: ifr 2010]

T. Souanef, F. Pinchetti, and W. Fichter. L1 Adaptive Control for Systems with Matched Stochastic Disturbance. Advances in Aerospace Guidance, Navigation and Control, 297-313, Srpinger, Berlin Heidelberg, 2013. [PUMA: ifr 2013]

M. Casasco, G. Saavedra, Criado, S. Weikert, J. Eggert, M. Hirth, T. Ott, and H. Su. Pointing Error Budgeting for High Pointing Accuracy Mission using the Pointing Error Engineering Tool. AIAA Guidance, Navigation, and Control Conference, (AIAA-2013-5251)Boston, Massachusetts, USA, Aug 19, 2013. [PUMA: ifr 2013]

J.-B. Maurice, F. A. King, and W. Fichter. Derivation and Validation of a Helicopter Rotor Model with Trailing Edge Flaps. Journal of Guidance, Control, and Dynamics, 2014. [PUMA: ifr 2014]

Jonathan Grzymisch, and Walter Fichter. Observability Criteria and Unobservable Maneuvers for In-Orbit Bearings-Only Navigation. Journal of Guidance, Control, and Dynamics, 2014. [PUMA: ifr 2014]

D. Gerardi, G. Allen, J. W. Conklin, K.-X. Sun, D. DeBra, S. Buchman, P. Gath, W. Fichter, R. L. Byer, and U. Johann. Advanced Drag-Free Concepts for Future Space-Based Interferometers: Acceleration Noise Budget. Review of Scientific Instruments, (85)January 2014. [PUMA: ifr 2014]

Tobias Ziegler, Patrick Bergner, Gerald Hechenblaikner, Nico Brandt, and Walter Fichter. Modeling and Performance of Contact-Free Discharge Systems for Space Inertial Sensors. IEEE Trans. Aerospace and Electronic Systems, 2014. [PUMA: ifr 2014]

M. Trittler, T. Rothermel, and W. Fichter. Visual Servoing Based Landing Approach Controller for Fixed-Wing MAVs. IFAC Symposium on Automatic Control in Aerospace, (19):September, Würzburg, Germany, February 2013. [PUMA: ifr 2013]

A. Steinwandel, and W. Fichter. Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction. Virginia Beach, Virginia, (71)Virginia Beach, Virginia, May 2015. [PUMA: ifr 2015]

Werner Grimm, and W. Rotärmel. Integrated Guidance and Control for Entry Vehicles. In P. Rentrop M. H. Breitner, G. Denk (Eds.), From Nano to Space - Applied Mathematics Inspired by Roland Bulirsch, Springer, 2008. [PUMA: 2008 ifr]

Jonathan Grzymisch, and Walter Fichter. Optimal Rendezvous Guidance with Enhanced Bearings-Only Observability. Journal of Guidance, Control, and Dynamics, Apr 20, 2015. [PUMA: ifr 2015]

Michael Frangenberg, Johannes Stephan, and Walter Fichter. Fast Actuator Fault Detection and Reconfiguration for Multicopters. AIAA Guidance, Navigation, and Control Conference, (AIAA 2015-1766)Kissimmee, Florida, Jan 8, 2015. [PUMA: ifr 2015]

T. Hablowetz, T. Mannchen, and Klaus. H. Well. Advanced Helicopter Flight Simulation with Controller in the Loop. Proceedings of the European Rotorcraft Forum, Netherlands Congress Centre, (26)25Hague, Netherlands, Sep 26, 2001. [PUMA: ifr 2001]

Adrien Grynagier, Walter Fichter, and Stefano Vitale. The Drift Mode for LISA Pathfinder: Implementation Solutions for a Robust Algorithm. Classical and Quantum Gravity, (26)9May 7, 2009. [PUMA: 2009 ifr]

Alexander Joos, Christop Seiferth, Lorenz Schmitt, and Walter Fichter. Parameters for Nonlinear Model Predictive Control in Unmanned Aerial Vehicle Path-Planning Applications. Journal of Guidance, Control, and Dynamics, The American Institute of Aeronautics and Astronautics, Aug 9, 2016. [PUMA: 2016 ifr] URL

Martin Hewitson, M Armano, M Benedetti, J Bogenstahl, D Bortoluzzi, P Bosetti, N Brandt, A Cavalleri, G Ciani, I Cristofolini, and others. Data analysis for the LISA Technology Package. Classical and Quantum Gravity, (26)9:094003, IOP Publishing, 2009. [PUMA: 2009 precision ifr]

F Antonucci, M Armano, H Audley, G Auger, M Benedetti, P Binetruy, C Boatella, J Bogenstahl, D Bortoluzzi, P Bosetti, and others. LISA Pathfinder: mission and status. Classical and Quantum Gravity, (28)9:094001, IOP Publishing, 2011. [PUMA: journal precision ifr 2011]

Frank King, Alexander Steinwandel, and Walter Fichter. Application Issues for In-Flight Tracking Control Using Trailing Edge Flaps. AHS - Forum 72 Proceedings, AHS International, Inc., West Palm Beach, Florida, USA, 2016. [PUMA: ifr]

Jonathan Grzymisch, and Walter Fichter. Nonlinear Pseudo-Measurement Filtering for In-Orbit Bearings-Only Navigation. IEEE Transactions on Aerospace and Electronic Systems, (51)4:2747 – 2759, 2015. [PUMA: ifr 2015]

Werner Grimm, and Klaus H. Well. Optimal Guidance Anticipating Missile Performance. AGARD-Symposium of the Guidance and Control Panel on Air Vehicle Mission Co, (53)Amsterdam, Netherlands, Oct 22, 1991. [PUMA: ifr 1991]