Publications

Thomas Mannchen, and Klaus H. Well. $\mu$-Analysis of Stability Margin Criteria. In Christopher Fielding, Andras Varga, Samir Bennani, and Michiel Selier (Eds.), Advanced Techniques for Clearance of Flight Control Laws, 285--311, Springer Berlin Heidelberg, Berlin, Heidelberg, 2002. [PUMA: ifr] URL

G. Weirich, and Werner Grimm. A Classical Approach Towards the Ascent Control of a Hypersonic Vehicle. Workshop des SFB 255: Optimalsteuerungsprobleme von Hyperschall-Flugsystemen, Tagungsband, 51-62, University Greifswald, Germany, October 1998. [PUMA: 1998 ifr]

G. Weirich, and Werner Grimm. A Classical Approach Towards the Ascent Control of a Hypersonic Vehicle. Workshop des SFB 255: Optimalsteuerungsprobleme von Hyperschall-Flugsystemen, Tagungsband, 51-62, University Greifswald, Germany, October 1998. [PUMA: ifr]

Lorenz Schmitt, and Walter Fichter. A Collision Avoidance Framework for Small Fixed-Wing Unmanned Aerial Vehicles. Journal of Guidance, Control, and Dynamics, (37)4Jun 25, 2014. [PUMA: ifr]

Lorenz Schmitt, and Walter Fichter. A Collision Avoidance Framework for Small Fixed-Wing Unmanned Aerial Vehicles. Journal of Guidance, Control, and Dynamics, May 19, 2014. [PUMA: ifr 2014]

Michael Paus. A General Approach to Optimal Real-Time Guidance of Dynamic Systems Based on Nonlinear Programming. AIAA Guidance, Navigation, and Control Conference, 92-43781992. [PUMA: ifr]

Michael Paus. A General Approach to Optimal Real-Time Guidance of Dynamic Systems Based on Nonlinear Programming. AIAA Guidance, Navigation, and Control Conference, 92-43781992. [PUMA: ifr 1992]

E. Wallner, J. Burkhardt, F. Zimmermann, U. M. Schöttle, and Klaus. H. Well. A Guidance and Control Concept for the X-38 Reentry Vehicle. International Astronautical Congress, (50)Amsterdam, Netherlands, 1999. [PUMA: ifr]

E. Wallner, J. Burkhardt, F. Zimmermann, U. M. Schöttle, and Klaus. H. Well. A Guidance and Control Concept for the X-38 Reentry Vehicle. International Astronautical Congress, (50)Amsterdam, Netherlands, 1999. [PUMA: 1999 ifr]

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, 215-231, Springer, 2013. [PUMA: ifr 2013]

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

Adam Vigneron, Simon Delchambre, Tobias Ziegler, and Walter Fichter. A Transient-Suppressing Initialization for Low-Bandwidth Attitude Controllers. Proceedings of the AIAA Scitech 2021 Forum, American Institute of Aeronautics and Astronautics, January 2021. [PUMA: ifr] URL

David Bamber, Jason Forshaw, Thomas Frame, Guglielmo Aglietti, Ramin Geshnizjani, Simon Goerries, Andrei Kornienko, Jens Levenhagen, Yang Gao, and Abadi Chanik. Absolute Attitude Determination System for a Spherical Air Bearing Testbed. 66th International Astronautical Congress, October 2015. [PUMA: myown conference iFR 2015]

David Bamber, Jason Forshaw, Thomas Frame, Guglielmo Aglietti, Ramin Geshnizjani, Simon Goerries, Andrei Kornienko, Jens Levenhagen, Yang Gao, and Abadi Chanik. Absolute Attitude Determination System for a Spherical Air Bearing Testbed. Proceedings of the 66th International Astronautical Congress, October 2015. [PUMA: ifr]

Johannes Stephan, and Walter Fichter. Active Battery Charge Drift Stabilization for Redundant Multirotors. Proceedings of the AIAA Scitech 2020 Forum, American Institute of Aeronautics and Astronautics, January 2020. [PUMA: ifr] URL

Florian Weimer, Thomas Rothermel, and Walter Fichter. Adaptive actuator fault detection and identification for UAV applications. Embedded Guidance, Navigation and Control in Aerospace, (1)1:67--72, International Federation of Automatic Control, Bangalore, India, February 2012. [PUMA: ifr 2012]

Florian Weimer, Thomas Rothermel, and Walter Fichter. Adaptive actuator fault detection and identification for UAV applications. Proceedings of the 1st IFAC Workshop on Embedded Guidance, Navigation and Control in Aerospace, International Federation of Automatic Control, Bangalore, India, February 2012. [PUMA: ifr]

Toufik Souanef, and Walter Fichter. Adaptive Altitude Hold of a Small Fixed Wing UAV. IFAC Symposium on Automatic Control in Aerospace, (19)Würzburg, Germany, Sep 2, 2013. [PUMA: ifr 2013]

Toufik Souanef, and Walter Fichter. Adaptive Altitude Hold of a Small Fixed Wing UAV. Proceedings of the 19th IFAC Symposium on Automatic Control in Aerospace 2013, (19)Sep 2, 2013. [PUMA: ifr]

M. Gräßlin, E. Wallner, J. Burkhardt, U. Schoettle, and 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]