Publications

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

F Antonucci, M Armano, H Audley, G Auger, M Benedetti, P Binetruy, C Boatella, J Bogenstahl, D Bortoluzzi, P Bosetti, und others. LISA Pathfinder data analysis. Classical and Quantum Gravity, (28)9:094006, IOP Publishing, 2011. [PUMA: journal jo precision ifr 2011]

F Antonucci, M Armano, H Audley, G Auger, M Benedetti, P Binetruy, C Boatella, J Bogenstahl, D Bortoluzzi, P Bosetti, und others. From laboratory experiments to LISA Pathfinder: achieving LISA geodesic motion. Classical and Quantum Gravity, (28)9:094002, IOP Publishing, 2011. [PUMA: precision ifr 2011]

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

M Armano, H Audley, G Auger, JT Baird, M Bassan, P Binetruy, M Born, D Bortoluzzi, N Brandt, M Caleno, und 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 Armano, M Benedetti, J Bogenstahl, D Bortoluzzi, P Bosetti, N Brandt, A Cavalleri, G Ciani, I Cristofolini, AM Cruise, und others. LISA Pathfinder: the experiment and the route to LISA. Classical and Quantum Gravity, (26)9:094001, IOP Publishing, 2009. [PUMA: 2009 precision ifr]

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

Wassef Ayadi, und Daniel Y. Reber. Helicopter Vibration Reduction Using Digitally Redesigned H-Infinity Controller in Observer Form. International Basic Research Conference on Rotorcraft Technology, (2)Nanjing, China, 07.11.2005. [PUMA: 2005 ifr]

John T. Betts, und Sven O. Erb. Computing Optimal Low Thrust Trajectories to the Moon. Proc. of the ESA Intern. Conf. on Spacecraft Guidance, Navig. & Contr.Systems, (5):143-163, 2002. [PUMA: ifr 2002]

Christoph Boehm, Moritz Merk, Walter Fichter, und Frank Allgöwer. Spacecraft Rate Damping with Predictive Control Using Magnetic Actuators Only. International Workshop on Assessment and Future Directions of NMPC, Pavia, Italy, 05.09.2008. [PUMA: 2008 ifr]

Nico Brandt, und Walter Fichter. Results and Consequences for the LISA Pathfinder Inertial Sensor FEM Analysis. Journal of Physics Conference Series, 7th International LISA Symposium, Barcelona, Spain, 16.06.2008. [PUMA: 2008 ifr]

M. H. Breitner, H. J. Pesch, und W. Grimm. Complex Differential Games of Pursuit-Evasion Type with State Constraints. Necessary Conditions for Optimal Open-Loop Strategies Journal of Optimization Theory and Applications, (78)3:419 - 441, September 1993. [PUMA: ifr 1993]

Wolfgang Buhl, Klaus Ebert, Heinrich Herbst, Klaus Schnepper, und Klaus. H. Well. Branched Trajectory Optimization for a Two-Stage to Orbit Vehicle. SIAM Conference on Numerical Analysis, Seattle, USA, 1993. [PUMA: ifr 1993]

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

M. Casasco, G. Saavedra, Criado, S. Weikert, J. Eggert, M. Hirth, T. Ott, und 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, 19.08.2013. [PUMA: ifr 2013]

Eugene M. Cliff, Klaus H. Well, und Klaus Schnepper. Flight-Test Guidance for Airbreathing Hypersonic Vehicles. NASA Center: Langley Research Center, Grant NAG-1-1244, 01.01.1992. [PUMA: ifr 1992]

Christian Dries, Walter Fichter, Alexander Joos, Ingmar Mayerbuch, Peter Müller, Federico Pinchetti, Reinhard Reichel, Rolf-Rekke Riebeling, Johannes Stephan, und Martin Volck. Automatischer Start und Landung einer Diamond DA42, Technologien der Universität Stuttgart. DGLR Netzpublikation, Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, Juli 2016. [PUMA: 2016 article]

M. Dìaz-Aguillò, A. Grynagier, B. Rais, M. Hewitson, M. Hueller, M. Nofrarias, L. Ferraioli, A. Monsky, M. Armano, A. Lobo, und E. Garcìa. Modeling LISA Pathfinder for Data Analysis. Journal of Physics Conference Series, 8th International LISA Symposium, Stanford University, CA, USA, 28.06.2010. [PUMA: ifr 2010]

S. Erb. Optimization of a GTO-GEO Low Thrust Satellite Transfer under Industrial Considerations. SIAM Conference on Optimization, Stockholm, Sweden, 2005. [PUMA: 2005 ifr]

Sven Oliver Erb, und John T. Betts. Optimal Low Thrust Trajectories to the Moon. SIAM J. Applied Dynamical Systems, 144-170, 2003. [PUMA: ifr 2003]

Martin Fach, Klaus H. Well, Uwe Salomon, und Florian Weimer. Camera-Aided Navigation Sensor for Unmanned Blimp with low Trajectory Dynamics. AIAA Guidance, Navigation, and Control Conference, Toronto, Ontario Canada, 02.08.2010. [PUMA: ifr 2010]

Walter Fichter, Peter Gath, Stefano Vitale, und Daniele Bortoluzzi. LISA Pathfinder drag-free control and system implications. Classical and Quantum Gravity, (22)10:S139, IOP Publishing, 2005. [PUMA: journal precision 2005 ifr]

Walter Fichter, Alexander Schleicher, Samir Bennani, und Shufan Wu. Closed Loop Performance and Limitations of the LISA Pathfinder Drag-Free Control System. AIAA Guidance Navigation and Control Conference, Hilton Head, South Carolina, USA, 20.08.2007. [PUMA: 2007 ifr]

Walter Fichter, Alexander Schleicher, und Stefano Vitale. Drag-Free Control Design with Cubic Test Masses. In H.J. Dittus, C. Lämmerzahl, und S. Turyshev (Hrsg.), Lasers, Clocks, and Drag-Free Control, (349)December2007. [PUMA: 2007 ifr]

Achim Figgen, A. J. Roenneke, und Klaus. H Well. Investigations of Guidance and Control of a Semi-Ballistic Reentry Vehicle. Space Course, (3):209-229, Universität Stuttgart, IFR, Stuttgart, Germany, 1995. [PUMA: 1995 ifr]

Denis Fischer, Till Zöbelein, und Axel Roenneke. Flugführung und Flugregelung des Deorbitmanövers von X-38/CRV. DGLR-Jahrbuch, 2001. [PUMA: ifr 2001]

Michael Frangenberg, Johannes Stephan, und Walter Fichter. Fast Actuator Fault Detection and Reconfiguration for Multicopters. AIAA Guidance, Navigation, and Control Conference, (AIAA 2015-1766)Kissimmee, Florida, 08.01.2015. [PUMA: ifr 2015]

P. F. Gath, und A. J. Calise. Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs. AIAA Guidance, Navigation, and Control Conference, (AIAA-99-4308)Portland, Oregon, USA, 09.08.1999. [PUMA: 1999 ifr]

P. F. Gath, Klaus. H. Well, und K. Mehlem. Automatic Initial Guess Generation for Ariane 5 Dual Payload Ascent Trajectory Optimization. AIAA Guidance, Navigation, and Control Conference, (AIAA 2000-4589)Denver, CO, USA, 14.08.2000. [PUMA: ifr 2000]

Peter Friedrich Gath, und 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]

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

Carlo Gerboni, Stefano Geluardi, Walter Fichter, und Heinrich Bülthoff. Investigation and Evaluation of Control Design Requirements for future Personal Aerial Vehicles. Fort Worth, Texas, Mai 2017. [PUMA: 2017 ifr]

Carlo Gerboni, Joost Venrooij, Frank Nieuwenhuizen, Alexander Joos, und Walter Fichter. Control Augmentation Strategies for Helicopters used as Personal Aerial Vehicles. AIAA Modeling and Simulation Technologies Conference, The American Institute of Aeronautics and Astronautics, Curran, Red Hook, New York, USA, Januar 2016. [PUMA: 2016 ifr]

Carlo Andrea Gerboni, Stefano Geluardi, Joost Venrooij, Alexander Joos, Walter Fichter, und Heinrich Buelthoff. Development of Model-Following Control Laws for Helicopters to achieve Personal Aerial Vehicle’s Handling Qualities. AIAA Modeling and Simulation Technologies Conference, accepted for publication, AIAA Science and Technology Forum and Exposition 2017, Grapevine, Texas, USA, Januar 2017. [PUMA: 2017 ifr]

F. Graf, T. Ott, J. P. Lejault, und W. Fichter. Precision pointing estimator design for minimum absolute, window- and stability-time errors. IFAC Symposium on Automatic Control in Aerospace, (19)Würzburg, Germany, 02.09.2013. [PUMA: ifr 2013]

Werner Grimm. On Ascent Guidance of a Hypersonic Vehicle. IFAC-Symposium on Automatic Control in Aerospace Control, (12)Ottobrunn, Germany, 07.09.1993. [PUMA: ifr 1993]

Werner Grimm. Optimal Flight Paths with Constrained Dynamic Pressure. In R. Bulirsch et al. (Hrsg.), Optimal Control - Calculus of Variations, Optimal Control Theory, and Numerical Methods, (111)Birkhäuser, Basel, Switzerland, 1993. [PUMA: ifr 1993]

Werner Grimm, C. Belle, und G. Fons. Fuel-Optimal Ascent of a Hypersonic Vehicle. Optimalsteuerung und Variationsrechnung - Optimal Control, Oberwolfach, Germany, 21.01.1996. [PUMA: 1996 ifr]

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

Werner Grimm, Christian Jänsch, Albert Markl, Klaus Schnepper, und Klaus Hinrich Well. Guidance of Aerospace Vehicles. Trajectory Optimization and Guidance of Aerospace Vehicles, DR 4.04 of the Carl-Cranz-GesellschaftOberpfaffenhofen, Germany, 1991. [PUMA: ifr 1991]

Werner Grimm, und A. Markl. Adjoint Estimation from a Direct Multiple Shooting Method". JOTA, (92)2Februar 1997. [PUMA: 1997 ifr]

Werner Grimm, und A. Markl. How to Estimate Adjoints from a Direct Multiple Shooting Method. JOTA Journal of Optimization Theory and Applications, 1995. [PUMA: 1995 ifr]

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

Werner Grimm, T. Stäbler, E. Wallner, A. Wiegand, R. da Costa, A. J. Roenneke, und G. Ortega. Unified Guidance and Control for Planetary Entry. International Symposium on Atmospheric Reentry Vehicles and Systems, (3)Arcachon, France, 24.03.2003. [PUMA: ifr 2003]

Werner Grimm, J. G. van der Meulen, und A. J. Roenneke. An Optimal Update Scheme for Drag Reference Profiles in an Entry Guidance. Journal of Guidance, Control, and Dynamics, (26)5:695-701, September 2003. [PUMA: ifr 2003]

Werner Grimm, und Klaus H. Well. Optimal Guidance Anticipating Missile Performance. AGARD-Symposium of the Guidance and Control Panel on Air Vehicle Mission Co, (53)Amsterdam, Netherlands, 22.10.1991. [PUMA: ifr 1991]

Werner Grimm, und Klaus. H. Well. Intercept Maneuvers with Reduced Detection Probability. DERA, Farnborough, UK, 17.03.1997. [PUMA: 1997 ifr]

Werner Grimm, und S. Zegoulli. Optimal Control of a Capsule in the Super-/Subsonic Region. ICIAM 95 - International Congress on Industrial and Applied Mathematics, Hamburg, Germany, 03.07.1995. [PUMA: 1995 ifr]

M. Gros, A. Schoettl, und 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, 19.08.2013. [PUMA: ifr 2013]

Michael Gros, Werner Grimm, Alfred Schöttl, und Walter Fichter. Finite receding-horizon incremental-sampling tree with application to a fixed-wing UAV. Embedded Guidance, Navigation and Control in Aerospace, (1)1:91--96, International Federation of Automatic Control, Bangalore, India, Februar 2012. [PUMA: ifr 2012]

A. Grynagier, S. Vitale, und W. Fichter. The Data Analysis for the LISA Pathfinder Drift Mode. Journal of Physics Conference Series, 8th International LISA Symposium, Stanford University, CA, USA, 28.06.2010. [PUMA: ifr 2010]

Adrien Grynagier, Walter Fichter, und Stefano Vitale. The Drift Mode for LISA Pathfinder: Implementation Solutions for a Robust Algorithm. Classical and Quantum Gravity, (26)907.05.2009. [PUMA: 2009 ifr]

Adrien Grynagier, Walter Fichter, und Stefano Vitale. Parabolic Drag-Free Flight, Actuation with Kicks, Spectral Analysis with Gaps. Space Science Reviews, (151)1-3Springer, 2010. [PUMA: ifr 2010]

Adrien Grynagier, Tobias Ziegler, und Walte Fichter. Identification of Dynamic Parameters for a One-Axis Drag-Free Gradiometer. IEEE Transactions on Aerospace and Electronic Systems, (49):341 - 355, 01.01.2013. [PUMA: ifr 2013]

J. Grzymisch, W. Fehse, W. Fichter, M. Casasco, und D. Losa. On the Issues and Requirements of Bearings-Only Guidance and Navigation for In-Orbit Rendezvous. International Astronautical Congress, (64)Beijing, China, 2013. [PUMA: ifr 2013]

J. Grzymisch, und W. Fichter. Analytic Optimal Observability Maneuvers for In-Orbit Bearings-Only Rendezvous. Journal of Guidance, Control and Dynamics., 27 Maarch 2014. [PUMA: ifr 2014]

J. Grzymisch, W. Fichter, M. Casasco, und D. Losa. A Spherical Coordinate Parameterization for an In-Orbit Bearings-Only Navigation Filter. Advances in Aerospace Guidance, Navigation and Control, 215-231, Springer, 2013. [PUMA: ifr 2013]

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

Jonathan Grzymisch, und Walter Fichter. Optimal Rendezvous Guidance with Enhanced Bearings-Only Observability. Journal of Guidance, Control, and Dynamics, 20.04.2015. [PUMA: ifr 2015]

Jonathan Grzymisch, und 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]

Jonathan Grzymisch, Walther Fichter, W. D. Losa, und M. Casasco. Bearings-Only Rendezvous with Enhanced Performance. Advances in Aerospace Guidance, Navigation and Control, 571-590, Springer, 2015. [PUMA: ifr 2015]

M. Gräßlin, E. Wallner, J. Burkhardt, U. Schoettle, und K. H. Well. Adaptive Guidance and Control Algorithms Applied to the X-38 Reentry Mission. International Astronautical Congress, Housten, Texas, USA, 2002. [PUMA: ifr 2002]

Norbert Haala, Michael Cramer, Florian Weimer, und Martin Trittler. Performance Test on UAV-Based Photogrammetric Data Collection. UAV-g (unmanned aerial vehicle in geomatics) Conference, Zurich, Switzerland, 14.09.2011. [PUMA: ifr 2011]

T. Hablowetz. Advanced Helicopter Flight and Aeroelastic Simulation based on General Purpose Multibody Code. AIAA Modeling and Simulation Technologies Conference, (AIAA 2000-4299)Denver, CO, USA, 14.08.2000. [PUMA: ifr 2000]

T. Hablowetz, T. Mannchen, und Klaus. H. Well. Advanced Helicopter Flight Simulation with Controller in the Loop. Proceedings of the European Rotorcraft Forum, Netherlands Congress Centre, (26)25Hague, Netherlands, 26.09.2001. [PUMA: ifr 2001]

Martin Hanel, und Klaus. H. Well. Optimierte Sensorpositionierung zur Regelung elastischer Strukturen. DGLR Jahrestagung, Munich, Germany, 14.10.1997. [PUMA: 1997 ifr]

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

M. Hirth, N. Brandt, und 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]

Marc Hirth, Walter Fichter, Nico Brandt, Alexander Schleicher, Domenico Gerardi, und Gudrun Wanner. Optical Metrology Alignment and Impact on the Measurement Performance of the LISA Technology Package. Journal of Physics Conference Series, 7th International LISA Symposium, Barcelona, Spain, 16.06.2008. [PUMA: 2008 ifr]

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

A. Joos, und W. Fichter. Parallel Implementation of Constrained Nonlinear Model Predictive Controller for an FPGA-based Onboard Flight Computer,. Advances in Aerospace Guidance, Navigation and Control, 273-286, Springer, 2011. [PUMA: ifr 2011]

A. Joos, M. A. Müller, D. Baumgärtner, W. Fichter, und F. Allgöwer. Nonlinear Predictive Control Based on Time-Domain Simulation for Automatic Landing. AIAA Guidance Navigation and Control Conference, Portland, Oregon, USA, 08.08.2011. [PUMA: ifr 2011]

A. Joos, F. Weimer, und W. Fichter. Path Planning with FPGAs for UAV Applications. Proceedings of the ESA GNC Conference, (8)Carlsbad, Czech Republic, 05.06.2011. [PUMA: ifr 2011]

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]

Alexander Joos, und Walter Fichter. Yaw Guidance for Airships under low Airspeed Conditions. AIAA Guidance Navigation and Control Conference, Toronto, Canada, 02.08.2010. [PUMA: ifr 2010]

Alexander Joos, Andy Häfner, Florian Weimer, und Walter Fichter. Quadrocopter Ground Effect Compensation with Sliding Mode Control. AIAA Guidance Navigation and Control Conference, Toronto, Canada, 02.08.2010. [PUMA: ifr 2010]

Alexander Joos, Pierre Heritier, Christoph Huber, und Walter Fichter. Method for parallel FPGA implementation of nonlinear model predictive control. Embedded Guidance, Navigation and Control in Aerospace, (1)1:73--78, International Federation of Automatic Control, Bangalore, India, Februar 2012. [PUMA: ifr 2012]

Alexander Joos, Christop Seiferth, Lorenz Schmitt, und 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, 09.08.2016. [PUMA: 2016 ifr] URL

C Jänsch, Klaus Schnepper, und KH Well. Multi-phase trajectory optimization methods with applications to hypersonic vehicles. Applied Mathematics in Aerospace Science and Engineering, 133--164, Springer, 1994. [PUMA: 1994 ifr]

Christian Jänsch, und Well Klaus H.. Optimal Multi-Criteria Aeroassisted Orbital Transfer Trajectories. IFACS Symposium on Automatic Control in Aerospace, (13)12.09.1994. [PUMA: 1994 ifr]

F. A. King, J.-B. Maurice, W. Fichter, O. Dieterich, und P. Konstanzer. In-Flight Rotorblade Tracking Control for Helicopters Using Active Trailing-Edge Flaps. Journal of Guidance, Control, and Dynamics, (37):633-643, 2014. [PUMA: ifr 2014]

F. A. King, J.-B. Maurice, W. Fichter, O. Dieterich, und P. Konstanzer. In-Flight Tracking Control for Helicopters using Active Trailing Edge Flaps. AIAA Guidance, Navigation, and Control Conference, (AIAA-2012-4443)Minneapolis, Minnesota, USA, 2012. [PUMA: ifr 2012]

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

Frank King, Alexander Steinwandel, und 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]

Hansjörg Klotz, M. Markus, W. Grimm, und S. E. Strandmoe. Guidance and Control for Autonomous Reentry and Precision Landing of a small Capsule. ESA International Conference on Spacecraft Guidance, Navigation, and Control, (4)Noordwijk, Netherlands, 1999. [PUMA: 1999 ifr]

Hansjörg Klotz, J. Starke, B. Frapard, C. Champetier, W. Grimm, und S. E. Strandmoe. Guidance, Navigation, and Control for Autonomous Reentry and Precision Landing of future small Capsules. AAF International Symposium on Atmospheric Reentry Vehicles and System, Arachon, France, 1999. [PUMA: 1999 ifr]

Thomas Kopfstedt, Marc-Oliver Restle, und Werner Grimm. Terrain Optimized Nonholonomic Following of Vehicle Tracks. IFAC Symposium on Intelligent Autonomous Vehicles, (7)Lecce, Italy, 06.09.2010. [PUMA: ifr 2010]

A. Kornienko, und K. Well. Estimation of Longitudinal Motion of a Remotely Controlled Airship. AIAA Atmospheric Flight Mechanics Conference, (AIAA-2003-5697)Austin, Texas, USA, August 2003. [PUMA: ifr 2003]

B. G. Kämpf, und Klaus. H. Well. Dynamics and Control of a Small Airship. International Airship Conference, (2)Friedrichshafen, Germany, Juni 1996. [PUMA: 1996 ifr]

B. G. Kämpf, und Klaus. H. Well. Attitude Control System for a Remotely-Controlled Airship. AIAA Lighter-Than-Air Systems Technology Conference, (11)Clearwater, Fl, USA, Mai 1995. [PUMA: 1995 ifr]

Reimund Küke, Peter Müller, Sebastian Polenz, Reinhard Reichel, Federico Pinchetti, Johannes Stephan, Alexander Joos, und Walter Fichter. Fly-By-Wire for CS23 Aircraft - Core Technology for General Aviation and RPAS. aerodays 2015, London, UK, Oktober 2016. [PUMA: 2016 ifr]

Gros M., Niendorf M., Schöttl A., und W. Fichter. Motion Planning for a Fixed-Wing MAV Incorporating Closed-Loop Dynamics Motion Primitives and Safety Maneuvers. Advances in Aerospace Guidance, Navigation and Control, 247-260, Springer, Berlin, 2011. [PUMA: ifr 2011]

T. Mannchen, D. G. Bates, und I Postlethwaite. Modeling and Computation of Worst-Case Uncertainty Combinations for Flight Control Systems Analysis. AIAA Journal of Guidance, Navigation, and Control, (25)62002. [PUMA: ifr 2002]

T. Mannchen, D. G. Bates, und I. Postlethwaite. Worst-Case Uncertain Parameter Combinations for Flight Control Systems Analysis. Proceedings of the IFAC World Congress, (15)1210Barcelona, Spain, 21.07.2002. [PUMA: ifr 2002]

T. Mannchen, und Klaus. H. Well. Helicopter Vibration Reduction using Periodic Robust Control. Proceedings of the AIAA Guidance, Navigation, and Control Conference, (AIAA-2001-4034)Montreal, Quebec, Canada, 06.08.2001. [PUMA: ifr 2001]

T. Mannchen, und Klaus. H. Well. μ-Analysis of Stability Margin Criteria. Control and Information Sciences, Advanced Techniques for Clearance of Flight Control Laws, (283/2002)Springer, 01.01.2002. [PUMA: ifr 2002]

T. Mannchen, und Klaus. H. Well. Influence of the Number of Rotor Blades on Helicopter Active Vibration Reduction Potential. Proceedings of the European Rotorcraft Forum, (28)81Bristol, UK, 17.09.2002. [PUMA: ifr 2002]

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

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

J.-B. Maurice, F. A. King, W. Fichter, A. Rabourdin, und P. K. Konstanzer. Helicopter Rotor In-Plane Stability Enhancement Using Trailing-Edge Flaps. Journal of Guidance, Control, and Dynamics, 2014. [PUMA: ifr 2014]