Publications

T. Mannchen, and Klaus. H. Well. μ-Analysis of Stability Margin Criteria. Control and Information Sciences, Advanced Techniques for Clearance of Flight Control Laws, (283/2002)Springer, Jan 1, 2002. [PUMA: ifr 2002]

Alexander Joos, and Walter Fichter. Yaw Guidance for Airships under low Airspeed Conditions. AIAA Guidance Navigation and Control Conference, Toronto, Canada, Aug 2, 2010. [PUMA: ifr 2010]

T. Mannchen, D. G. Bates, and I. Postlethwaite. Worst-Case Uncertain Parameter Combinations for Flight Control Systems Analysis. Proceedings of the IFAC World Congress, (15)1210Barcelona, Spain, Jul 21, 2002. [PUMA: ifr 2002]

Klaus. H. Well, and Axel J. Roenneke. Vom Weltraum aufs Fußballfeld - geht das?. Jahrbuch Universität Stuttgart, 1994. [PUMA: 1994 ifr]

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]

Werner Grimm, T. Stäbler, E. Wallner, A. Wiegand, R. da Costa, A. J. Roenneke, and G. Ortega. Unified Guidance and Control for Planetary Entry. International Symposium on Atmospheric Reentry Vehicles and Systems, (3)Arcachon, France, Mar 24, 2003. [PUMA: ifr 2003]

Thomas Mannchen, and Klaus H. Well. Uncertainty Bands Approach to LFT Modelling. In C. Fielding, A. Varga, S. Bennani, and M. Selier (Eds.), Advanced Techniques for Clearance of Flight Control Laws, (283/2002)Springer, 2002. [PUMA: ifr 2002]

Alexander Joos. Unbemannte Fluggeräte: Vorteile, Anwendungen und technische Herausforderungen. Ausgezeichnete Forschungsbeiträge 2013, Stiftung Werner-von-Siemens-Ring, 42-49, VDE Verlag, 2015. [PUMA: ifr 2015]

Peter Friedrich Gath, and Klaus H. Well. Trajectory Optimization Using a Combination of Direct Multiple Shooting and Collocation. AIAA Guidance, Navigation, and Control Conference, (AIAA-2001-4047)2001. [PUMA: ifr 2001]

Axel Roenneke, Klaus Schütz, and Klaus. H. Well. Trajectory Optimization Using 6-DOF Vehicle Models. IFAC Workshop on Control Applications of Optimization, (10)Haifa, Israel, 1995. [PUMA: 1995 ifr]

A. J. Roenneke, and P. J. Cornwell. Trajectory Control for a Low-Lift Reentry Vehicle. Journal of Guidance, Control, and Dynamics, (16)5:927 - 933, September 1993. [PUMA: ifr 1993]

Werner Grimm, and M. Hans. Time-Optimal Turn to a Heading: the Complete Analytic Solution. Journal of Guidance, Control, and Dynamics, (21)61998. [PUMA: 1998 ifr]

F Antonucci, M Armano, H Audley, G Auger, M Benedetti, P Binetruy, J Bogenstahl, D Bortoluzzi, P Bosetti, N Brandt, and others. The lisa pathfinder mission. Classical and Quantum Gravity, (29)12:124014, IOP Publishing, 2012. [PUMA: journal precision ifr 2012]

H Audley, K Danzmann, G Heinzel, A Monsky, M Nofrarias, F Steier, D Gerardi, R Gerndt, G Hechenblaikner, U Johann, and others. The LISA Pathfinder interferometry? hardware and system testing. Classical and Quantum Gravity, (28)9:094003, IOP Publishing, 2011. [PUMA: precision ifr 2011]

A Monsky, M Hewitson, L Ferraioli, Gudrun Wanner, Miquel Nofrarias, M Hueller, I Diepholz, A Grynagier, M Armano, M Benedetti, and others. The first mock data challenge for LISA Pathfinder. Classical and Quantum Gravity, (26)9:094004, IOP Publishing, 2009. [PUMA: 2009 precision ifr]

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]

A. Grynagier, S. Vitale, and W. Fichter. The Data Analysis for the LISA Pathfinder Drift Mode. Journal of Physics Conference Series, 8th International LISA Symposium, Stanford University, CA, USA, Jun 28, 2010. [PUMA: ifr 2010]

Elmar M. Wallner, and Klaus H. Well. TETRA Technologien für zukünftige Raumtransportsysteme Improved X-38 Flight Control and Simulation. AIAA Guidance, Navigation, and Control Conference, 2003. [PUMA: ifr 2003]

Elmar M. Wallner, and Klaus H. Well. TETRA Technologien für zukünftige Raumtransportsysteme Anpassung der Lageregelung der X-38 an eine neue Version der Aerodynamik. AIAA Guidance, Navigation, and Control Conference, 2003. [PUMA: ifr 2003]

Tobias Ziegler, and Walter Fichter. Test Mass Stiffness Estimation for the LISA Pathfinder Drag-Free System. AIAA Guidance Navigation and Control Conference, Hilton Head, South Carolina, USA, Aug 20, 2007. [PUMA: 2007 ifr]

Thomas Kopfstedt, Marc-Oliver Restle, and Werner Grimm. Terrain Optimized Nonholonomic Following of Vehicle Tracks. IFAC Symposium on Intelligent Autonomous Vehicles, (7)Lecce, Italy, Sep 6, 2010. [PUMA: ifr 2010]

M Armano, H Audley, G Auger, JT Baird, M Bassan, P Binetruy, M Born, D Bortoluzzi, N Brandt, M Caleno, and others. Sub-Femto-g Free Fall for Space-Based Gravitational Wave Observatories: LISA Pathfinder Results. Physical Review Letters, (116)23:231101, APS, 2016. [PUMA: 2016 ifr]

M. Gros, A. Schoettl, and W. Fichter. Spline and OBB-based Path-Planning for Small UAVs with the Finite Receding-Horizon Incremental-Sampling Tree Algorithm. AIAA Guidance, Navigation, and Control Conference, (AIAA 2013-4788)Boston, Massachusetts, USA, Aug 19, 2013. [PUMA: ifr 2013]

Christoph Boehm, Moritz Merk, Walter Fichter, and Frank Allgöwer. Spacecraft Rate Damping with Predictive Control Using Magnetic Actuators Only. International Workshop on Assessment and Future Directions of NMPC, Pavia, Italy, Sep 5, 2008. [PUMA: 2008 ifr]

C. Böhm, M. Merk, W. Fichter, and F. Allgöwer. Spacecraft Rate Damping with Predictive Control using Magnetic Actuators Only. In K. Magni, and F. Allgöwer (Eds.), Nonlinear Model Predictive Control - Towards New Challenging Applications, Lecture Notes in Control and Information Sciences, 511-520, Springer, 2009. [PUMA: 2009 ifr]

Lorenz Schmitt, and Walter Fichter. Smooth Singularity Free Solution to the Three-Dimensional Bearings-Only Tracking Problem. AIAA Guidance, Navigation, and Control Conference, 1858, The American Institute of Aeronautics and Astronautics, San Diego, California, USA, January 2016. [PUMA: 2016 ifr]

Fabio Montemurro, Walter Fichter, and Markus Schlotterer. Sliding Mode Technique Applied to Test Mass Suspension Control. IFAC Aerospace Symposium, Toulouse, France, Jun 25, 2007. [PUMA: 2007 ifr]

Tilo Reubelt, Nico Sneeuw, Siavash Iran-Pour, Walter Fichter, and Marc Hirth. Sensitivity Analysis of Future Satellite Formations and Configurations of them. April 2011. [PUMA: ifr 2011]

Florian Saupe, Jean-Baptiste Maurice, Frank King, and Walter Fichter. Robustness Analysis of Linear Time Periodic Systems using Harmonic Transfer Function. AIAA GNC Conference, Chicago, USA, Aug 10, 2009. [PUMA: 2009 ifr]

Axel J. Roenneke. Robuste Bahnfolgeregelung für den Wiedereintritt von Kapseln. Deutsche Luft- und Raumfahrtkongress, Oct 14, 1997. [PUMA: 1997 ifr]

Jean-Baptiste Maurice, Roberto Farolfi, Florian Saupe, Frank A. King, and Walter Fichter. Robust Stability Analysis of a Linear Time-Periodic Active Helicopter Rotor. AIAA Journal of Guidance, Control, and Dynamics, (35)5:1625-1636, 2012. [PUMA: ifr 2012]

M. Trittler, W. Fichter, and A. Schöttl. Return Strategies for Fixed-Wing MAVs after Loss of GPS. IFAC Symposium on Automatic Control in Aerospace, (19)Würzburg, Germany, Sep 2, 2013. [PUMA: ifr 2013]

Nico Brandt, and Walter Fichter. Results and Consequences for the LISA Pathfinder Inertial Sensor FEM Analysis. Journal of Physics Conference Series, 7th International LISA Symposium, Barcelona, Spain, Jun 16, 2008. [PUMA: 2008 ifr]

Jörg Schuler, and Klaus. H. Well. Reglerentwurf für eine integrale Flugmechanik- und Aeroelastikregelung eines Großraumflugzeuges. DGLR Jahrestagung, Dresden, Germany, Sep 24, 1996. [PUMA: 1996 ifr]

Axel J. Roenneke, and A. Markl. Reentry Control to a Drag-vs-Energy Profile. Journal of Guidance, Control and Dynamics, (17)5:916-920, 1993. [PUMA: ifr 1993]

A. J. Roenneke, and Klaus. H. Well. Reentry Control of a Low-Lift Maneuverable Spacecraft. AIAA Guidance, Navigation, and Control Conference, (AIAA 92-4455-CP):641 - 652, Hilton Head, South Carolina, USA, 1992. [PUMA: ifr 1992]

M. Paus, Werner Grimm, and Klaus. H. Well. Real-Time Optimization for the Guidance of Dynamic Systems. IFAC Workshop on Control Applications of Optimization, (10)Haifa, Israel, Dec 19, 1995. [PUMA: 1995 ifr]

M. Paus, Werner Grimm, and Klaus. H. Well. Real-Time Optimisation for the Guidance of Dynamic Systems. In H. Neunzert (Eds.), Progress in Industrial Mathematics at ECMI 94, Teubner, Leipzig, Germany, 1996. [PUMA: 1996 ifr]

Alexander Joos, Andy Häfner, Florian Weimer, and Walter Fichter. Quadrocopter Ground Effect Compensation with Sliding Mode Control. AIAA Guidance Navigation and Control Conference, Toronto, Canada, Aug 2, 2010. [PUMA: ifr 2010]

Tobias Ziegler, Walter Fichter, Markus Schulte, and Stefano Vitale. Principles, Operations, and Expected Performance of the LISA Pathfinder Charge Management System. Journal of Physics Conference Series, 7th International LISA Symposium, Barcelona, Spain, Jun 16, 2008. [PUMA: 2008 ifr]

Martin Trittler, Walter Fichter, Rudof Voit-Nitschmann, Robert Schmoldt, and Klaus Kittmann. Preliminary System Identification of the Blended Wing Body Flight Demonstrator VELA2 from Flight Data. AIAA Atmospheric Flight Mechanics Conference, Honolulu, USA, Aug 18, 2008. [PUMA: 2008 ifr]

Rainer Saage, Alexander Schleicher, and Walter Fichter. Predicted Drag-Free Performance of LISA Pathfinder and Operational Optimization Means. 8th International LISA Symposium, Stanford University, USA, July 2010. [PUMA: ifr 2010]

Ott T., Fichter W., Bennani S., and Winkler S.. Precision Pointing H∞ Control Design for Absolute, Window-, and Stability-Time Errors. CEAS Space Journal, Springer, 2013. [PUMA: ifr 2013]

F. Graf, T. Ott, J. P. Lejault, and W. Fichter. Precision pointing estimator design for minimum absolute, window- and stability-time errors. IFAC Symposium on Automatic Control in Aerospace, (19)Würzburg, Germany, Sep 2, 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]

F. Weimer, M. Frangenberg, and W. Fichter. Pipelined Particle Filter with Nonobservability Measure for Attitude and Velocity Estimation. Journal of Guidance, Control, and Dynamics, Apr 14, 2014. [PUMA: ifr 2014]

F. Weimer, M. Frangenberg, and W. Fichter. Pipelined Particle Filter with Non-Observability Measure for On-Board Navigation with MAVs. AIAA Guidance, Navigation, and Control Conference, (AIAA-2013-5247)Boston, Massachusetts, USA, Aug 19, 2013. [PUMA: ifr 2013]

Norbert Haala, Michael Cramer, Florian Weimer, and Martin Trittler. Performance Test on UAV-Based Photogrammetric Data Collection. UAV-g (unmanned aerial vehicle in geomatics) Conference, Zurich, Switzerland, Sep 14, 2011. [PUMA: ifr 2011]

F. A. King, A. Steinwandel, and W. Fichter. Performance Characteristics of Symmetrized In-Flight Tracking Control. AHS Annual Forum, (70)Quebec, Canada, May 2014. [PUMA: ifr 2014]

Marc Hirth, Walter Fichter, Tilo Reubelt, Nico Sneeuw, and Siavash Iran-Pour. Performance Aspects of Future Gravity Mission Constellations. April 2011. [PUMA: ifr 2011]