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Yaw Guidance for Airships under low Airspeed Conditions. AIAA Guidance Navigation and Control Conference, Toronto, Canada, Aug 2, 2010. [PUMA: ifr 2010]
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]
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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]
Unified Guidance and Control for Planetary Entry. International Symposium on Atmospheric Reentry Vehicles and Systems, (3)Arcachon, France, Mar 24, 2003. [PUMA: ifr 2003]
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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]
Terrain Optimized Nonholonomic Following of Vehicle Tracks. IFAC Symposium on Intelligent Autonomous Vehicles, (7)Lecce, Italy, Sep 6, 2010. [PUMA: ifr 2010]
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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]
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Sliding Mode Technique Applied to Test Mass Suspension Control. IFAC Aerospace Symposium, Toulouse, France, Jun 25, 2007. [PUMA: 2007 ifr]
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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]
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]
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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]
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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]
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]
Predicted Drag-Free Performance of LISA Pathfinder and Operational Optimization Means. 8th International LISA Symposium, Stanford University, USA, July 2010. [PUMA: ifr 2010]
Precision Pointing H∞ Control Design for Absolute, Window-, and Stability-Time Errors. CEAS Space Journal, Springer, 2013. [PUMA: ifr 2013]
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]
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]
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