Publications

Bookshelf

 

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All Publications

  1. 2017

    1. J. Stephan and W. Fichter, “Fast Exact Redistributed Pseudoinverse Method for Linear Actuation Systems,” IEEE Transactions on Control Systems Technology, 2017.
    2. L. Schmitt and W. Fichter, “Cramér-Rao Lower Bound for State-Constrained Nonlinear Filtering,” IEEE Signal Processing Letters, vol. 24, no. 12, 2017.
    3. A. Kornienko, P. Dhole, R. Geshnizjani, P. Jamparueang, and W. Fichter, “Determing Spacecraft Moment of Inertia using In-Orbit Data,” in 10th International ESA Conference on Guidance, Navigation & Control Systems, Salzburg, Austria, 2017.
    4. C. Gerboni, S. Geluardi, W. Fichter, and H. Bülthoff, “Investigation and Evaluation of Control Design Requirements for future Personal Aerial Vehicles,” Fort Worth, Texas, 2017.
    5. A. Schleicher, Z. Ziegler, R. Schubert, U. Johann, W. Fichter, and J. Grzymisch, “In-Orbit Performance of the LISA Pathfinder Drag Free and Attitude Control System,” 2017.
    6. C. A. Gerboni, S. Geluardi, J. Venrooij, A. Joos, W. Fichter, and H. 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, 2017.
  2. 2016

    1. S. Notter, A. Heckmann, A. McFadyen, and L. Gonzalez, “Modelling, Simulation and Flight Tests of a Model Predictive Controlled Multirotor with Heavy Slung Load,” in IFAC Symposium on Automatic Control in Aerospace, Sherbrooke, Canada, 2016, vol. 20.
    2. F. King, A. Steinwandel, and W. Fichter, “Application Issues for In-Flight Tracking Control Using Trailing Edge Flaps,” AHS - Forum 72 Proceedings, 2016.
    3. M. Trittler, T. Rothermel, and W. Fichter, “Autopilot for Landing Small Fixed-Wing Unmanned Aerial Vehicles with Optical Sensors,” Journal of Guidance, Control, and Dynamics, vol. 39, pp. 2011–2021, 2016.
    4. A. Posch, B. Fuchs, J. Renkl, J. Sommer, A. O. Schwientek, and W. Fichter, “Close-Range 3D Collision Prediction under Attitude Uncertainty for On-Orbit Servicing Missions,” in IFAC Symposium on Automatic Control in Aerospace, Sherbrooke, Canada, 2016, vol. 20.
    5. C. Dries, W. Fichter, A. Joos, I. Mayerbuch, P. Müller, F. Pinchetti, R. Reichel, R.-R. Riebeling, J. Stephan, and M. Volck, “Automatischer Start und Landung einer Diamond DA42, Technologien der Universität Stuttgart,” DGLR Netzpublikation, 2016.
    6. L. Schmitt and W. Fichter, “Continuous Singularity Free Approach to the Three-Dimensional Bearings-Only Tracking Problem,” Journal of Guidance, Control, and Dynamics, vol. 39, no. 12, pp. 2673–2682, 2016.
    7. R. Geshnizjani, A. Kornienko, and W. Fichter, “Angular Momentum Based Steering Approach for Control Moment Gyroscopes,” in 20th IFAC Symposium on Automatic Control in Aerospace, Sherbrooke, Canada, 2016.
    8. A. Kornienko, J. Rieber, T. Ott, R. Geshnizjani, W. Fichter, J. Forshaw, and G. Aglietti, “Experimental Verification of Attitude Control System for Agile Spacecraft,” in 20th IFAC Symposion on Automatic Control in Aerospace, Sherbrooke, Canada, 2016.
    9. M. Armano, H. Audley, G. Auger, J. 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, vol. 116, no. 23, p. 231101, 2016.
    10. F. Pinchetti, J. Stephan, A. Joos, and W. Fichter, “FlySmart - Automatic Take-Off and Landing of an EASA CS-23 Aircraft,” in Deutscher Luft- und Raumfahrtkongress 2016, 2016.
    11. A. Joos, C. Seiferth, L. Schmitt, and W. Fichter, “Parameters for Nonlinear Model Predictive Control in Unmanned Aerial Vehicle Path-Planning Applications,” Journal of Guidance, Control, and Dynamics, 2016.
    12. C. Seiferth, A. Joos, M. Frangenberg, and W. Fichter, “Predictive Motion Planning with Pipelined Feature-Based Obstacle Avoidance,” Journal of Guidance, Control and Dynamics, vol. 39, no. 4, pp. 970–978, 2016.
    13. R. Küke, P. Müller, S. Polenz, R. Reichel, F. Pinchetti, J. Stephan, A. Joos, and W. Fichter, “Fly-By-Wire for CS23 Aircraft - Core Technology for General Aviation and RPAS,” in aerodays 2015, London, UK, 2016.
    14. L. Schmitt and W. Fichter, “Smooth Singularity Free Solution to the Three-Dimensional Bearings-Only Tracking Problem,” in AIAA Guidance, Navigation, and Control Conference, San Diego, California, USA, 2016, p. 1858.
    15. T. Rath, T. Richter, A. Steinwandel, and W. Fichter, “Emulation of Whirl Flutter on a Stable Helicopter Using Trailing Edge Flaps,” in AHS - Forum 72 Proceedings, West Palm Beach, Florida, USA, 2016.
    16. C. Gerboni, J. Venrooij, F. Nieuwenhuizen, A. Joos, and W. Fichter, “Control Augmentation Strategies for Helicopters used as Personal Aerial Vehicles,” AIAA Modeling and Simulation Technologies Conference, 2016.
    17. J. Stephan and W. Fichter, “Fast Generation of Landing Paths for Fixed-Wing Aircraft with Thrust Failure,” AIAA Guidance, Navigation, and Control Conference, vol. AIAA 2016–1874, 2016.
  3. 2015

    1. D. Bamber, J. Forshaw, T. Frame, G. Aglietti, R. Geshnizjani, S. Goerries, A. Kornienko, J. Levenhagen, Y. Gao, and A. Chanik, “Absolute Attitude Determination System for a Spherical Air Bearing Testbed,” in 66th International Astronautical Congress, 2015.
    2. A. Joos, “Unbemannte Fluggeräte: Vorteile, Anwendungen und technische Herausforderungen,” in Ausgezeichnete Forschungsbeiträge 2013, Stiftung Werner-von-Siemens-Ring, VDE Verlag, 2015, pp. 42–49.
    3. M. Frangenberg, J. Stephan, and W. Fichter, “Fast Actuator Fault Detection and Reconfiguration for Multicopters,” AIAA Guidance, Navigation, and Control Conference, vol. AIAA 2015–1766, 2015.
    4. J. Grzymisch and W. Fichter, “Optimal Rendezvous Guidance with Enhanced Bearings-Only Observability,” Journal of Guidance, Control, and Dynamics, 2015.
    5. J. Grzymisch, W. Fichter, W. D. Losa, and M. Casasco, “Bearings-Only Rendezvous with Enhanced Performance,” Advances in Aerospace Guidance, Navigation and Control, pp. 571–590, 2015.
    6. T. Souanef, A. Boubakir, and W. Fichter, “L1 Adaptive Control of Systems with Disturbances of Unknown Bounds,” Advances in Aerospace Guidance, Navigation and Control, pp. 151–165, 2015.
    7. T. Souanef and W. Fichter, “Fault Tolerant L1 Adaptive Control Based on Degraded Models,” Advances in Aerospace Guidance, Navigation and Control, no. 135–149, 2015.
    8. N. Wildmann, M. Hofsäß, F. Weimer, A. Joos, and J. Bange, “MASC - a small Remotely Piloted Aircraft (RPA) for wind energy research,” Advances in Science and Research, pp. 55–61, 2015.
    9. T. Richter, T. Rath, O. Oberinger, and W. Fichter, “Investigation of Whirl Flutter Stabilization using Active Trailing Edge Flaps,” AHS Annual Forum, vol. 71, 2015.
    10. 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, vol. 71, 2015.
    11. J. Grzymisch and W. Fichter, “Nonlinear Pseudo-Measurement Filtering for In-Orbit Bearings-Only Navigation,” IEEE Transactions on Aerospace and Electronic Systems, vol. 51, no. 4, pp. 2747 – 2759, 2015.
    12. L. Schmitt and W. Fichter, “Observability Criteria and Null-Measurement Kalman Filter for Vision-Aided Inertial Navigation,” Journal of Guidance, Control, and Dynamics, 2015.
  4. 2014

    1. A. Posch, M. Schmidt, A. O. Schwientek, J. Sommer, and W. Fichter, “Real-Time 3D Collision Prediction for On-Orbit Servicing Missions,” in IFAC World Congress, Capetown, South Africa, 2014.
    2. L. Schmitt and W. Fichter, “A Collision Avoidance Framework for Small Fixed-Wing Unmanned Aerial Vehicles,” Journal of Guidance, Control, and Dynamics, 2014.
    3. J. Grzymisch and W. Fichter, “Analytic Optimal Observability Maneuvers for In-Orbit Bearings-Only Rendezvous,” Journal of Guidance, Control and Dynamics., 2014.
    4. T. Ziegler, P. Bergner, G. Hechenblaikner, N. Brandt, and W. Fichter, “Modeling and Performance of Contact-Free Discharge Systems for Space Inertial Sensors,” IEEE Trans. Aerospace and Electronic Systems, 2014.
    5. 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, vol. 85, 2014.
    6. J. Grzymisch and W. Fichter, “Observability Criteria and Unobservable Maneuvers for In-Orbit Bearings-Only Navigation,” Journal of Guidance, Control, and Dynamics, 2014.
    7. F. Weimer, M. Frangenberg, and W. Fichter, “Pipelined Particle Filter with Nonobservability Measure for Attitude and Velocity Estimation,” Journal of Guidance, Control, and Dynamics, 2014.
    8. J.-B. Maurice, F. A. King, W. Fichter, A. Rabourdin, and P. K. Konstanzer, “Helicopter Rotor In-Plane Stability Enhancement Using Trailing-Edge Flaps,” Journal of Guidance, Control, and Dynamics, 2014.
    9. 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.
    10. F. A. King, J.-B. Maurice, W. Fichter, O. Dieterich, and P. Konstanzer, “In-Flight Rotorblade Tracking Control for Helicopters Using Active Trailing-Edge Flaps,” Journal of Guidance, Control, and Dynamics, vol. 37, pp. 633–643, 2014.
    11. F. A. King, A. Steinwandel, and W. Fichter, “Performance Characteristics of Symmetrized In-Flight Tracking Control,” AHS Annual Forum, vol. 70, 2014.
  5. 2013

    1. A. Posch, A. O. Schwientek, J. Sommer, and W. Fichter, “Model-Based On-Board Realtime Thruster Fault Monitoring,” in IFAC Symposium on Automatic Control in Aerospace, Würzburg, Germany, 2013, vol. 19.
    2. J. Grzymisch, W. Fichter, M. Casasco, and D. Losa, “A Spherical Coordinate Parameterization for an In-Orbit Bearings-Only Navigation Filter,” Advances in Aerospace Guidance, Navigation and Control, pp. 215–231, 2013.
    3. T. Souanef, F. Pinchetti, and W. Fichter, “L1 Adaptive Control for Systems with Matched Stochastic Disturbance,” Advances in Aerospace Guidance, Navigation and Control, pp. 297–313, 2013.
    4. O. T., F. W., B. S., and W. S., “Precision Pointing H∞ Control Design for Absolute, Window-, and Stability-Time Errors,” CEAS Space Journal, 2013.
    5. A. Grynagier, T. Ziegler, and W. Fichter, “Identification of Dynamic Parameters for a One-Axis Drag-Free Gradiometer,” IEEE Transactions on Aerospace and Electronic Systems, vol. 49, pp. 341 – 355, 2013.
    6. J. Grzymisch, W. Fehse, W. Fichter, M. Casasco, and D. Losa, “On the Issues and Requirements of Bearings-Only Guidance and Navigation for In-Orbit Rendezvous,” International Astronautical Congress, vol. 64, 2013.
    7. M. Trittler, T. Rothermel, and W. Fichter, “Visual Servoing Based Landing Approach Controller for Fixed-Wing MAVs,” IFAC Symposium on Automatic Control in Aerospace, vol. 19, p. September, Feb. 2013.
    8. M. Trittler, W. Fichter, and A. Schöttl, “Return Strategies for Fixed-Wing MAVs after Loss of GPS,” IFAC Symposium on Automatic Control in Aerospace, vol. 19, 2013.
    9. A. Posch, A. O. Schwientek, J. Sommer, and W. Fichter, “Model-Based On-Board Realtime Thruster Fault Monitoring,” IFAC Symposium on Automatic Control in Aerospace, vol. 19, 2013.
    10. 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, vol. 19, 2013.
    11. T. Souanef and W. Fichter, “Adaptive Altitude Hold of a Small Fixed Wing UAV,” IFAC Symposium on Automatic Control in Aerospace, vol. 19, 2013.
    12. 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, vol. AIAA 2013–4788, 2013.
    13. 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, vol. AIAA-2013–5251, 2013.
    14. H. Vogel, W. Fichter, R. Choe, E. Xargay, and N. Hovakimyan, “Magnetic Momentum Control of a Satellite Augmented with an L1 Adaptive Controller,” AIAA Guidance, Navigation, and Control Conference, vol. AIAA 2013–5092, 2013.
    15. 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, vol. AIAA-2013–5247, 2013.
  6. 2012

    1. A. Posch, A. O. Schwientek, J. Sommer, and W. Fichter, “Comparison of filter techniques for relative state estimation of in-orbit servicing missions,” in IFAC Workshop eGNC in Aerospace, Bangalore, India, 2012.
    2. 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, vol. 29, no. 12, p. 124014, 2012.
    3. A. Joos, P. Heritier, C. Huber, and W. Fichter, “Method for parallel FPGA implementation of nonlinear model predictive control,” in Embedded Guidance, Navigation and Control in Aerospace, Bangalore, India, 2012, vol. 1, no. 1, pp. 73–78.
    4. F. Weimer, T. Rothermel, and W. Fichter, “Adaptive actuator fault detection and identification for UAV applications,” in Embedded Guidance, Navigation and Control in Aerospace, Bangalore, India, 2012, vol. 1, no. 1, pp. 67–72.
    5. M. Gros, W. Grimm, A. Schöttl, and W. Fichter, “Finite receding-horizon incremental-sampling tree with application to a fixed-wing UAV,” in Embedded Guidance, Navigation and Control in Aerospace, Bangalore, India, 2012, vol. 1, no. 1, pp. 91–96.
    6. R. Saage, R. Ross, W. Fichter, and A. Schleicher, “Closed-Loop Specifications for Spacecraft Control Under Micropropulsion Constraints,” AIAA Journal of Guidance, Control, and Dynamics, vol. 35, no. 5, pp. 1676–1681, 2012.
    7. J.-B. Maurice, R. Farolfi, F. Saupe, F. A. King, and W. Fichter, “Robust Stability Analysis of a Linear Time-Periodic Active Helicopter Rotor,” AIAA Journal of Guidance, Control, and Dynamics, vol. 35, no. 5, pp. 1625–1636, 2012.
    8. S. Weikert, A. Wiegand, W. Fichter, and R. Saage, “Coupled Mission and GNC Analysis for Space Robotic Missions”,” International Astronautical Congress, vol. 63, 2012.
    9. F. A. King, J.-B. Maurice, W. Fichter, O. Dieterich, and P. Konstanzer, “In-Flight Tracking Control for Helicopters using Active Trailing Edge Flaps,” AIAA Guidance, Navigation, and Control Conference, vol. AIAA-2012–4443, 2012.
  7. 2011

    1. 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, vol. 28, no. 9, p. 094003, 2011.
    2. F. Antonucci, M. Armano, H. Audley, G. Auger, M. Benedetti, P. Binetruy, C. Boatella, J. Bogenstahl, D. Bortoluzzi, P. Bosetti, and others, “From laboratory experiments to LISA Pathfinder: achieving LISA geodesic motion,” Classical and Quantum Gravity, vol. 28, no. 9, p. 094002, 2011.
    3. 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, vol. 28, no. 9, p. 094001, 2011.
    4. F. Antonucci, M. Armano, H. Audley, G. Auger, M. Benedetti, P. Binetruy, C. Boatella, J. Bogenstahl, D. Bortoluzzi, P. Bosetti, and others, “LISA Pathfinder data analysis,” Classical and Quantum Gravity, vol. 28, no. 9, p. 094006, 2011.
    5. T. Reubelt, N. Sneeuw, S. Iran-Pour, W. Fichter, and M. Hirth, “Sensitivity Analysis of Future Satellite Formations and Configurations of them.” 2011.
    6. M. Hirth, W. Fichter, T. Reubelt, N. Sneeuw, and S. Iran-Pour, “Performance Aspects of Future Gravity Mission Constellations.” 2011.
    7. A. Joos and W. Fichter, “Parallel Implementation of Constrained Nonlinear Model Predictive Controller for an FPGA-based Onboard Flight Computer,” Advances in Aerospace Guidance, Navigation and Control, pp. 273–286, 2011.
    8. G. M., N. M., S. A., and 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, pp. 247–260, 2011.
    9. M. Niendorf, M. Gros, A. Schöttl, and W. Fichter, “Local Planning for a Fixed-Wing MAV with a Tree-Based Planner and Motion Primitives,” DGLR Kongress, 2011.
    10. N. Haala, M. Cramer, F. Weimer, and M. Trittler, “Performance Test on UAV-Based Photogrammetric Data Collection,” UAV-g (unmanned aerial vehicle in geomatics) Conference, 2011.
    11. A. Joos, M. A. Müller, D. Baumgärtner, W. Fichter, and F. Allgöwer, “Nonlinear Predictive Control Based on Time-Domain Simulation for Automatic Landing,” AIAA Guidance Navigation and Control Conference, 2011.
    12. M. Trittler, H. Su, W. Fichter, and A. Schoettl, “Intelligent Camera as Subsystem for Vision-Aided On-Board Navigation of MAVs,” Proc. ESA GNC Conference, 2011.
    13. T. Ott, A. Benoit, P. Van den Braembussche, and W. Fichter, “ESA Pointing Error Engineering Handbook,” International ESA Conference on Guidance, Navigation & Control Systems, vol. 8, 2011.
    14. T. Ott, W. Fichter, S. Bennani, and S. Winkler, “Coherent Precision Pointing Control Design based on Hinf-Closed Loop Shaping,” International ESA Conference on Guidance, Navigation & Control Systems, vol. 8, 2011.
    15. S. Winkler, F. Cirillo, K. Ergenzinger, T. Ott, R. Wilhelm, and E. Zaunick, “High-Precision Attitude Determination and Control of the EUCLID Spacecraft: Challenges and Solutions,” International ESA Conference on Guidance, Navigation & Control Systems, vol. 8, 2011.
    16. A. Joos, F. Weimer, and W. Fichter, “Path Planning with FPGAs for UAV Applications,” Proceedings of the ESA GNC Conference, vol. 8, 2011.
  8. 2010

    1. R. Saage, A. Schleicher, and W. Fichter, “Predicted Drag-Free Performance of LISA Pathfinder and Operational Optimization Means.” 8th International LISA Symposium, Stanford University, USA, 2010.
    2. T. Ziegler, A. Schleicher, and W. Fichter, “Identification Algorithms for Micro-Propulsion System Parameters using Drag-Free Test Masses,” Space Science Reviews, vol. 151, no. 1–3, 2010.
    3. A. Grynagier, W. Fichter, and S. Vitale, “Parabolic Drag-Free Flight, Actuation with Kicks, Spectral Analysis with Gaps,” Space Science Reviews, vol. 151, no. 1–3, 2010.
    4. M. Hirth, N. Brandt, and W. Fichter, “Inertial Sensing for Future Gravity Missions,” GEOTECHNOLOGIEN Science Report, Observation of the System Earth from Space, no. 17, 2010.
    5. M. Fach, K. H. Well, U. Salomon, and F. Weimer, “Camera-Aided Navigation Sensor for Unmanned Blimp with low Trajectory Dynamics,” AIAA Guidance, Navigation, and Control Conference, 2010.
    6. M. Dìaz-Aguillò, A. Grynagier, B. Rais, M. Hewitson, M. Hueller, M. Nofrarias, L. Ferraioli, A. Monsky, M. Armano, A. Lobo, and E. Garcìa, “Modeling LISA Pathfinder for Data Analysis,” Journal of Physics Conference Series, 8th International LISA Symposium, 2010.
    7. 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, 2010.
    8. T. Kopfstedt, M.-O. Restle, and W. Grimm, “Terrain Optimized Nonholonomic Following of Vehicle Tracks,” IFAC Symposium on Intelligent Autonomous Vehicles, vol. 7, 2010.
    9. R. Saage, A. Schleicher, and W. Fichter, “Method for LFT Calculation with High Order Parametric Systems,” AIAA Guidance Navigation and Control Conference, 2010.
    10. R. Saage, R. Ross, A. Schleicher, and W. Fichter, “Controller Design Method for Drag-Free Systems with Micro-Propulsion Constraints,” AIAA Guidance Navigation and Control Conference, 2010.
    11. A. Joos, A. Häfner, F. Weimer, and W. Fichter, “Quadrocopter Ground Effect Compensation with Sliding Mode Control,” AIAA Guidance Navigation and Control Conference, 2010.
    12. F. Weimer, M. Trittler, A. Joos, M. Gros, A. Posch, and W. Fichter, “FPGA-Based Onboard Computer System for Mini Aerial Vehicles,” International Micro Air Vehicle Conference and Flight Competition, 2010.
    13. A. Joos and W. Fichter, “Yaw Guidance for Airships under low Airspeed Conditions,” AIAA Guidance Navigation and Control Conference, 2010.
  9. 2009

    1. A. Posch and S. Sukkarieh, “UAV based search for a radio tagged animal using particle filters,” in Australasian Conference on Robotics and Automation, Sydney, Australia, 2009.
    2. M. Armano, M. Benedetti, J. Bogenstahl, D. Bortoluzzi, P. Bosetti, N. Brandt, A. Cavalleri, G. Ciani, I. Cristofolini, A. Cruise, and others, “LISA Pathfinder: the experiment and the route to LISA,” Classical and Quantum Gravity, vol. 26, no. 9, p. 094001, 2009.
    3. M. 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, vol. 26, no. 9, p. 094003, 2009.
    4. A. Monsky, M. Hewitson, L. Ferraioli, G. Wanner, M. 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, vol. 26, no. 9, p. 094004, 2009.
    5. C. Böhm, M. Merk, W. Fichter, and F. Allgöwer, “Spacecraft Rate Damping with Predictive Control using Magnetic Actuators Only,” Nonlinear Model Predictive Control - Towards New Challenging Applications,  Lecture Notes in Control and Information Sciences, pp. 511–520, 2009.
    6. A. Grynagier, W. Fichter, and S. Vitale, “The Drift Mode for LISA Pathfinder: Implementation Solutions for a Robust Algorithm,” Classical and Quantum Gravity, vol. 26, no. 9, 2009.
    7. J.-B. Maurice, F. King, W. Fichter, O. Dieterich, and P. Konstanzer, “Floquet Convergence Analysis for Periodic Active Rotor Systems Equipped with Trailing Edge Flaps,” European Rotorcraft Forum, vol. 35, 2009.
    8. F. Saupe, J.-B. Maurice, F. King, and W. Fichter, “Robustness Analysis of Linear Time Periodic Systems using Harmonic Transfer Function,” AIAA GNC Conference, 2009.
  10. 2008

    1. W. Grimm and W. Rotärmel, “Integrated Guidance and Control for Entry Vehicles,” From Nano to Space - Applied Mathematics Inspired by Roland Bulirsch, 2008.
    2. M. Trittler, W. Fichter, R. Voit-Nitschmann, R. Schmoldt, and K. Kittmann, “Preliminary System Identification of the Blended Wing Body Flight Demonstrator VELA2 from Flight Data,” AIAA Atmospheric Flight Mechanics Conference, 2008.
    3. M. Hirth, W. Fichter, N. Brandt, A. Schleicher, D. Gerardi, and G. Wanner, “Optical Metrology Alignment and Impact on the Measurement Performance of the LISA Technology Package,” Journal of Physics Conference Series, 7th International LISA Symposium, 2008.
    4. T. Ziegler, W. Fichter, M. Schulte, and S. Vitale, “Principles, Operations, and Expected Performance of the LISA Pathfinder Charge Management System,” Journal of Physics Conference Series, 7th International LISA Symposium, 2008.
    5. N. Brandt and W. Fichter, “Results and Consequences for the LISA Pathfinder Inertial Sensor FEM Analysis,” Journal of Physics Conference Series, 7th International LISA Symposium, 2008.
    6. A. Schleicher, R. Saage, M. Hirth, N. Brandt, and W. Fichter, “Drag-Free Control Design for Misaligned Cubic Test Masses,” International ESA Conference on Guidance, Navigation & Control Systems, vol. 7, 2008.
    7. C. Boehm, M. Merk, W. Fichter, and F. Allgöwer, “Spacecraft Rate Damping with Predictive Control Using Magnetic Actuators Only,” International Workshop on Assessment and Future Directions of NMPC, 2008.
  11. 2007

    1. W. Fichter, A. Schleicher, and S. Vitale, “Drag-Free Control Design with Cubic Test Masses,” Lasers, Clocks, and Drag-Free Control, vol. 349, no. December, 2007.
    2. T. Ziegler, M. Göbel, A. Schleicher, and W. Fichter, “Calibration of the Micro-Newton Propulsion System of the LISA Pathfinder Drag-Free Satellite,” CEAS Conference, vol. 1, 2007.
    3. T. Ziegler and W. Fichter, “Test Mass Stiffness Estimation for the LISA Pathfinder Drag-Free System,” AIAA Guidance Navigation and Control Conference, 2007.
    4. W. Fichter, A. Schleicher, S. Bennani, and S. Wu, “Closed Loop Performance and Limitations of the LISA Pathfinder Drag-Free Control System,” AIAA Guidance Navigation and Control Conference, 2007.
    5. F. Montemurro, W. Fichter, and M. Schlotterer, “Sliding Mode Technique Applied to Test Mass Suspension Control,” IFAC Aerospace Symposium, 2007.
  12. 2006

    1. K. H. Well, “Aircraft Control Laws for Envelope Protection,” AIAA GNC Conference in Keystone, vol. AIAA 2006–6055, 2006.
    2. A. Mayanna, W. Grimm, and K. H. Well, “Adaptive Guidance for Terminal Area Energy Management (TAEM) of Reentry Vehicles,” AIAA GNC Conference in Keystone, vol. AIAA 2006–6037, 2006.

 

@2015 iFR - Flight Mechanics and Controls Lab

Address

Flight Mechanics and Controls Lab
Pfaffenwaldring 27
70569 Stuttgart
Germany

Contact

Phone:   +49 711 685-67061

Fax:        +49 711 685-66670

Mail:       ifr@ifr.uni-stuttgart.de