Publikationen

Alle Publikationen von 2004 bis heute

  1. 2020

    1. Notter, S., Groß, P., Schrapel, P., & Fichter, W. (2020). Multiple Thermal Updraft Estimation and Observability Analysis. Journal of Guidance, Control, and Dynamics, 43(3), 490–503. https://doi.org/10.2514/1.G004205
    2. Stephan, J., Notter, S., Pfeifle, O., Pinchetti, F., & Fichter, W. (2020). Spline Trajectory Planning and Guidance for Fixed-Wing Drones. AIAA Scitech 2020 Forum. https://doi.org/10.2514/6.2020-0372
  2. 2019

    1. Geshnizjani, Ramin, Kornienko, A., Ziegler, T., Loehr, J., & Fichter, W. (2019). Optimal Initial Gimbal Angles for Agile Slew Maneuvers with Control Moment Gyroscopes. AIAA Scitech 2019 Forum. https://doi.org/10.2514/6.2019-0936
    2. Groß, P., Notter, S., & Fichter, W. (2019). Estimating Total Energy Compensated Climb Rates from Position Trajectories. AIAA Scitech 2019 Forum. https://doi.org/10.2514/6.2019-0828
    3. Notter, S., Zürn, M., Groß, P., & Fichter, W. (2019). Reinforced Learning to Cross-Country Soar in the Vertical Plane of Motion. AIAA Scitech 2019 Forum. https://doi.org/10.2514/6.2019-1420
    4. Schmitt, L., & Fichter, W. (2019). Globally Valid Posterior Cramér-Rao Bound for Three-Dimensional Bearings-Only Filtering. IEEE Transactions on Aerospace and Electronic Systems, 55(4), 2036–2044. https://doi.org/10.1109/TAES.2018.2881352
    5. Stephan, J., Fichter, W., Yüksel, B., & Zwiener, J. (2019). Sicher über der Stadt, Volocopter und Universität Stuttgart entwickeln Flugsteuerungssystem für Flugtaxis. DGLR Magazin Luft- Und Raumfahrt.
  3. 2018

    1. Friedrich, M., & Fichter, W. (2018). Optimization of the mass ratio for a general multi-rotor aircraft. In 2018 AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0531
    2. Geiss, I., Notter, S., Strohmayer, A., & Fichter, W. (2018). Optimized Operation Strategies for Serial Hybrid-Electric Aircraft. 2018 Aviation Technology, Integration, and Operations Conference. https://doi.org/10.2514/6.2018-4230
    3. Geshnizjani, R., Freudenau, B., & Fichter, W. (2018). Scaled Verification Scenarios for Agile AOCS Testbeds. 67. Deutscher Luft- Und Raumfahrtkongress. https://doi.org/10.25967/480181
    4. Kazenmaier, U., Gerboni, C., Geluardi, S., Olivari, M., Richter, T., Fichter, W., & Bülthoff, H. H. (2018). Development of a civil light helicopter flight simulator for pilot training. Proceedings of the 44th European Rotorcraft Forum 2018 (ERF), 1197–1205.
    5. Notter, S., Schrapel, P., Groß, P., & Fichter, W. (2018). Estimation of Multiple Thermal Updrafts Using a Particle Filter Approach. In 2018 AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1854
    6. Pinchetti, F., Joos, A., & Fichter, W. (2018). Efficient Continuous Curvature Path Generation with Pseudo-Parameterized Algebraic Splines. CEAS Aeronautical Journal (Accepted for Publication).
    7. Schleicher, A, Ziegler, T., Schubert, R., Brandt, N., Bergner, P., Johann, U., Fichter, W., & Grzymisch, J. (2018). In-orbit performance of the LISA Pathfinder drag-free and attitude control system. CEAS Space Journal, 1–15.
    8. Stephan, J., & Fichter, W. (2018). Gain-Scheduled Multivariable Flight Control under Uncertain Trim Conditions. In 2018 AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1130
    9. Stephan, J., Schmitt, L., & Fichter, W. (2018). Linear Parameter-Varying Control for Quadrotors in Case of Complete Actuator Loss. Journal of Guidance, Control, and Dynamics, 1–15. https://doi.org/10.2514/1.G003441
  4. 2017

    1. Gerboni, C., Geluardi, S., Fichter, W., & Bülthoff, H. (2017). Investigation and Evaluation of Control Design Requirements for future Personal Aerial Vehicles.
    2. Gerboni, C. A., Geluardi, S., Venrooij, J., Joos, A., Fichter, W., & Buelthoff, H. (2017). 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.
    3. Kornienko, A., Dhole, P., Geshnizjani, R., Jamparueang, P., & Fichter, W. (2017). Determing Spacecraft Moment of Inertia using In-Orbit Data. 10th International ESA Conference on Guidance, Navigation & Control Systems.
    4. Schleicher, Alexander, Ziegler, Z., Schubert, R., Johann, U., Fichter, W., & Grzymisch, J. (2017). In-Orbit Performance of the LISA Pathfinder Drag-Free and Attitude Control System.
    5. Schmitt, Lorenz, & Fichter, W. (2017). Cramér-Rao Lower Bound for State-Constrained Nonlinear Filtering. IEEE Signal Processing Letters, 24(12), Article 12. https://doi.org/10.1109/LSP.2017.2764540
    6. Stephan, J., & Fichter, W. (2017). Fast Exact Redistributed Pseudoinverse Method for Linear Actuation Systems. IEEE Transactions on Control Systems Technology.
  5. 2016

    1. Armano, M., Audley, H., Auger, G., Baird, J., Bassan, M., Binetruy, P., Born, M., Bortoluzzi, D., Brandt, N., Caleno, M., & others. (2016). Sub-Femto-g Free Fall for Space-Based Gravitational Wave Observatories: LISA Pathfinder Results. Physical Review Letters, 116(23), 231101.
    2. Dries, C., Fichter, W., Joos, A., Mayerbuch, I., Müller, P., Pinchetti, F., Reichel, R., Riebeling, R.-R., Stephan, J., & Volck, M. (2016). Automatischer Start und Landung einer Diamond DA42, Technologien der Universität Stuttgart. DGLR Netzpublikation.
    3. Gerboni, C., Venrooij, J., Nieuwenhuizen, F., Joos, A., & Fichter, W. (2016). Control Augmentation Strategies for Helicopters used as Personal Aerial Vehicles. AIAA Modeling and Simulation Technologies Conference.
    4. Geshnizjani, Ramin, Kornienko, A., & Fichter, W. (2016). Angular Momentum Based Steering Approach for Control Moment Gyroscopes. 20th IFAC Symposium on Automatic Control in Aerospace.
    5. Joos, Alexander, Seiferth, C., Schmitt, L., & Fichter, W. (2016). Parameters for Nonlinear Model Predictive Control in Unmanned Aerial Vehicle Path-Planning Applications. Journal of Guidance, Control, and Dynamics. http://dx.doi.org/10.2514/1.G000311
    6. King, F., Steinwandel, A., & Fichter, W. (2016). Application Issues for In-Flight Tracking Control Using Trailing Edge Flaps. AHS - Forum 72 Proceedings.
    7. Kornienko, A., Rieber, J., Ott, T., Geshnizjani, R., Fichter, W., Forshaw, J., & Aglietti, G. (2016). Experimental Verification of Attitude Control System for Agile Spacecraft. 20th IFAC Symposion on Automatic Control in Aerospace.
    8. Küke, R., Müller, P., Polenz, S., Reichel, R., Pinchetti, F., Stephan, J., Joos, A., & Fichter, W. (2016). Fly-By-Wire for CS23 Aircraft - Core Technology for General Aviation and RPAS. Aerodays 2015.
    9. Notter, S., Heckmann, A., McFadyen, A., & Gonzalez, L. (2016). Modelling, Simulation and Flight Tests of a Model Predictive Controlled Multirotor with Heavy Slung Load. IFAC Symposium on Automatic Control in Aerospace, 20.
    10. Pinchetti, F., Stephan, J., Joos, A., & Fichter, W. (2016). FlySmart - Automatic Take-Off and Landing of an EASA CS-23 Aircraft. Deutscher Luft- Und Raumfahrtkongress 2016.
    11. Rath, T., Richter, T., Steinwandel, A., & Fichter, W. (2016). Emulation of Whirl Flutter on a Stable Helicopter Using Trailing Edge Flaps. AHS - Forum 72 Proceedings.
    12. Schmitt, Lorenz, & Fichter, W. (2016b). Smooth Singularity Free Solution to the Three-Dimensional Bearings-Only Tracking Problem. AIAA Guidance, Navigation, and Control Conference, 1858.
    13. Schmitt, Lorenz, & Fichter, W. (2016a). Continuous Singularity Free Approach to the Three-Dimensional Bearings-Only Tracking Problem. Journal of Guidance, Control, and Dynamics, 39(12), 2673--2682. https://doi.org/10.2514/1.G000362
    14. Stephan, J., & Fichter, W. (2016). Fast Generation of Landing Paths for Fixed-Wing Aircraft with Thrust Failure. AIAA Guidance, Navigation, and Control Conference, AIAA 2016-1874.
    15. Trittler, Martin, Rothermel, T., & Fichter, W. (2016). Autopilot for Landing Small Fixed-Wing Unmanned Aerial Vehicles with Optical Sensors. Journal of Guidance, Control, and Dynamics, 39, 2011–2021.
  6. 2015

    1. Bamber, D., Forshaw, J., Frame, T., Aglietti, G., Geshnizjani, R., Goerries, S., Kornienko, A., Levenhagen, J., Gao, Y., & Chanik, A. (2015). Absolute Attitude Determination System for a Spherical Air Bearing Testbed. 66th International Astronautical Congress.
    2. Frangenberg, M., Stephan, J., & Fichter, W. (2015). Fast Actuator Fault Detection and Reconfiguration for Multicopters. AIAA Guidance, Navigation, and Control Conference, AIAA 2015-1766.
    3. Grzymisch, Jonathan, & Fichter, W. (2015). Optimal Rendezvous Guidance with Enhanced Bearings-Only Observability. Journal of Guidance, Control, and Dynamics.
    4. Grzymisch, Jonathan, Fichter, W., Losa, W. D., & Casasco, M. (2015). Bearings-Only Rendezvous with Enhanced Performance. Advances in Aerospace Guidance, Navigation and Control, 571–590.
    5. Joos, Alexander. (2015). Unbemannte Fluggeräte: Vorteile, Anwendungen und technische Herausforderungen. In Ausgezeichnete Forschungsbeiträge 2013, Stiftung Werner-von-Siemens-Ring (pp. 42–49). VDE Verlag.
    6. Richter, T., Rath, T., Oberinger, O., & Fichter, W. (2015). Investigation of Whirl Flutter Stabilization using Active Trailing Edge Flaps. AHS Annual Forum, 71.
    7. Souanef, T., Boubakir, A., & Fichter, W. (2015). L1 Adaptive Control of Systems with Disturbances of Unknown Bounds. Advances in Aerospace Guidance, Navigation and Control, 151–165.
    8. Souanef, T., & Fichter, W. (2015). Fault Tolerant L1 Adaptive Control Based on Degraded Models. Advances in Aerospace Guidance, Navigation and Control, 135–149, Article 135–149.
    9. Steinwandel, A., & Fichter, W. (2015). Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction. Virginia Beach, Virginia, 71.
    10. Wildmann, N., Hofsäß, M., Weimer, F., Joos, A., & Bange, J. (2015). MASC - a small Remotely Piloted Aircraft (RPA) for wind energy research. Advances in Science and Research, 55–61.
  7. 2014

    1. Gerardi, D., Allen, G., Conklin, J. W., Sun, K.-X., DeBra, D., Buchman, S., Gath, P., Fichter, W., Byer, R. L., & Johann, U. (2014). Advanced Drag-Free Concepts for Future Space-Based Interferometers: Acceleration Noise Budget. Review of Scientific Instruments, 85.
    2. Grzymisch, J., & Fichter, W. (2014). Analytic Optimal Observability Maneuvers for In-Orbit Bearings-Only Rendezvous. Journal of Guidance, Control and Dynamics.
    3. Grzymisch, Jonathan, & Fichter, W. (2014). Observability Criteria and Unobservable Maneuvers for In-Orbit Bearings-Only Navigation. Journal of Guidance, Control, and Dynamics.
    4. King, F. A., Steinwandel, A., & Fichter, W. (2014). Performance Characteristics of Symmetrized In-Flight Tracking Control. AHS Annual Forum, 70.
    5. King, F. A., Maurice, J.-B., Fichter, W., Dieterich, O., & Konstanzer, P. (2014). In-Flight Rotorblade Tracking Control for Helicopters Using Active Trailing-Edge Flaps. Journal of Guidance, Control, and Dynamics, 37, 633–643.
    6. Maurice, J.-B., King, F. A., Fichter, W., Rabourdin, A., & Konstanzer, P. K. (2014). Helicopter Rotor In-Plane Stability Enhancement Using Trailing-Edge Flaps. Journal of Guidance, Control, and Dynamics.
    7. Maurice, J.-B., King, F. A., & Fichter, W. (2014). Derivation and Validation of a Helicopter Rotor Model with Trailing Edge Flaps. Journal of Guidance, Control, and Dynamics.
    8. Schmitt, Lorenz, & Fichter, W. (2014). A Collision Avoidance Framework for Small Fixed-Wing Unmanned Aerial Vehicles. Journal of Guidance, Control, and Dynamics.
    9. Weimer, F., Frangenberg, M., & Fichter, W. (2014). Pipelined Particle Filter with Nonobservability Measure for Attitude and Velocity Estimation. Journal of Guidance, Control, and Dynamics.
    10. Ziegler, T., Bergner, P., Hechenblaikner, G., Brandt, N., & Fichter, W. (2014). Modeling and Performance of Contact-Free Discharge Systems for Space Inertial Sensors. IEEE Trans. Aerospace and Electronic Systems.
  8. 2013

    1. Casasco, M., Saavedra, G., Criado, Weikert, S., Eggert, J., Hirth, M., Ott, T., & Su, H. (2013). Pointing Error Budgeting for High Pointing Accuracy Mission using the Pointing Error Engineering Tool. AIAA Guidance, Navigation, and Control Conference, AIAA-2013-5251.
    2. Graf, F., Ott, T., Lejault, J. P., & Fichter, W. (2013). Precision pointing estimator design for minimum absolute, window- and stability-time errors. IFAC Symposium on Automatic Control in Aerospace, 19.
    3. Gros, M., Schoettl, A., & Fichter, W. (2013). 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.
    4. Grynagier, A., Ziegler, T., & Fichter, W. (2013). Identification of Dynamic Parameters for a One-Axis Drag-Free Gradiometer. IEEE Transactions on Aerospace and Electronic Systems, 49, 341–355.
    5. Grzymisch, J., Fehse, W., Fichter, W., Casasco, M., & Losa, D. (2013). On the Issues and Requirements of Bearings-Only Guidance and Navigation for In-Orbit Rendezvous. International Astronautical Congress, 64.
    6. Grzymisch, J., Fichter, W., Casasco, M., & Losa, D. (2013). A Spherical Coordinate Parameterization for an In-Orbit Bearings-Only Navigation Filter. Advances in Aerospace Guidance, Navigation and Control, 215–231.
    7. Posch, A., Schwientek, A. O., Sommer, J., & Fichter, W. (2013). Model-Based On-Board Realtime Thruster Fault Monitoring. IFAC Symposium on Automatic Control in Aerospace, 19.
    8. Souanef, T., Pinchetti, F., & Fichter, W. (2013). L1 Adaptive Control for Systems with Matched Stochastic Disturbance. Advances in Aerospace Guidance, Navigation and Control, 297–313.
    9. Souanef, Toufik, & Fichter, W. (2013). Adaptive Altitude Hold of a Small Fixed Wing UAV. IFAC Symposium on Automatic Control in Aerospace, 19.
    10. T., O., W., F., S., B., & S., W. (2013). Precision Pointing H∞ Control Design for Absolute, Window-, and Stability-Time Errors. CEAS Space Journal.
    11. Trittler, M., Rothermel, T., & Fichter, W. (2013). Visual Servoing Based Landing Approach Controller for Fixed-Wing MAVs. IFAC Symposium on Automatic Control in Aerospace, 19, September.
    12. Trittler, M., Fichter, W., & Schöttl, A. (2013). Return Strategies for Fixed-Wing MAVs after Loss of GPS. IFAC Symposium on Automatic Control in Aerospace, 19.
    13. Vogel, H., Fichter, W., Choe, R., Xargay, E., & Hovakimyan, N. (2013). Magnetic Momentum Control of a Satellite Augmented with an L1 Adaptive Controller. AIAA Guidance, Navigation, and Control Conference, AIAA 2013-5092.
    14. Weimer, F., Frangenberg, M., & Fichter, W. (2013). Pipelined Particle Filter with Non-Observability Measure for On-Board Navigation with MAVs. AIAA Guidance, Navigation, and Control Conference, AIAA-2013-5247.
  9. 2012

    1. Antonucci, F., Armano, M., Audley, H., Auger, G., Benedetti, M., Binetruy, P., Bogenstahl, J., Bortoluzzi, D., Bosetti, P., Brandt, N., & others. (2012). The lisa pathfinder mission. Classical and Quantum Gravity, 29(12), 124014.
    2. Gros, Michael, Grimm, W., Schöttl, A., & Fichter, W. (2012). Finite receding-horizon incremental-sampling tree with application to a fixed-wing UAV. Embedded Guidance, Navigation and Control in Aerospace, 1(1), 91--96.
    3. Joos, Alexander, Heritier, P., Huber, C., & Fichter, W. (2012). Method for parallel FPGA implementation of nonlinear model predictive control. Embedded Guidance, Navigation and Control in Aerospace, 1(1), 73--78.
    4. King, F. A., Maurice, J.-B., Fichter, W., Dieterich, O., & Konstanzer, P. (2012). In-Flight Tracking Control for Helicopters using Active Trailing Edge Flaps. AIAA Guidance, Navigation, and Control Conference, AIAA-2012-4443.
    5. Maurice, Jean-Baptiste, Farolfi, R., Saupe, F., King, F. A., & Fichter, W. (2012). Robust Stability Analysis of a Linear Time-Periodic Active Helicopter Rotor. AIAA Journal of Guidance, Control, and Dynamics, 35(5), 1625–1636.
    6. Saage, R., Ross, R., Fichter, W., & Schleicher, A. (2012). Closed-Loop Specifications for Spacecraft Control Under Micropropulsion Constraints. AIAA Journal of Guidance, Control, and Dynamics, 35(5), 1676–1681.
    7. Weikert, S., Wiegand, A., Fichter, W., & Saage, R. (2012). Coupled Mission and GNC Analysis for Space Robotic Missions”. International Astronautical Congress, 63.
    8. Weimer, Florian, Rothermel, T., & Fichter, W. (2012). Adaptive actuator fault detection and identification for UAV applications. Embedded Guidance, Navigation and Control in Aerospace, 1(1), 67--72.
  10. 2011

    1. Antonucci, F., Armano, M., Audley, H., Auger, G., Benedetti, M., Binetruy, P., Boatella, C., Bogenstahl, J., Bortoluzzi, D., Bosetti, P., & others. (2011a). From laboratory experiments to LISA Pathfinder: achieving LISA geodesic motion. Classical and Quantum Gravity, 28(9), 094002.
    2. Antonucci, F., Armano, M., Audley, H., Auger, G., Benedetti, M., Binetruy, P., Boatella, C., Bogenstahl, J., Bortoluzzi, D., Bosetti, P., & others. (2011b). LISA Pathfinder: mission and status. Classical and Quantum Gravity, 28(9), 094001.
    3. Antonucci, F., Armano, M., Audley, H., Auger, G., Benedetti, M., Binetruy, P., Boatella, C., Bogenstahl, J., Bortoluzzi, D., Bosetti, P., & others. (2011c). LISA Pathfinder data analysis. Classical and Quantum Gravity, 28(9), 094006.
    4. Audley, H., Danzmann, K., Heinzel, G., Monsky, A., Nofrarias, M., Steier, F., Gerardi, D., Gerndt, R., Hechenblaikner, G., Johann, U., & others. (2011). The LISA Pathfinder interferometry? hardware and system testing. Classical and Quantum Gravity, 28(9), 094003.
    5. Hirth, M., Fichter, W., Reubelt, T., Sneeuw, N., & Iran-Pour, S. (2011). Performance Aspects of Future Gravity Mission Constellations.
    6. Joos, A., & Fichter, W. (2011). Parallel Implementation of Constrained Nonlinear Model Predictive Controller for an FPGA-based Onboard Flight Computer,. Advances in Aerospace Guidance, Navigation and Control, 273–286.
    7. M., G., M., N., A., S., & Fichter, W. (2011). 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.
    8. Niendorf, M., Gros, M., Schöttl, A., & Fichter, W. (2011). Local Planning for a Fixed-Wing MAV with a Tree-Based Planner and Motion Primitives. DGLR Kongress.
    9. Reubelt, T., Sneeuw, N., Iran-Pour, S., Fichter, W., & Hirth, M. (2011). Sensitivity Analysis of Future Satellite Formations and Configurations of them.
  11. 2010

    1. Grynagier, A., Fichter, W., & Vitale, S. (2010). Parabolic Drag-Free Flight, Actuation with Kicks, Spectral Analysis with Gaps. Space Science Reviews, 151(1–3), Article 1–3.
    2. Saage, R., Schleicher, A., & Fichter, W. (2010). Predicted Drag-Free Performance of LISA Pathfinder and Operational Optimization Means. 8th International LISA Symposium.
    3. Ziegler, T., Schleicher, A., & Fichter, W. (2010). Identification Algorithms for Micro-Propulsion System Parameters using Drag-Free Test Masses. Space Science Reviews, 151(1–3), Article 1–3.
  12. 2009

    1. Armano, M., Benedetti, M., Bogenstahl, J., Bortoluzzi, D., Bosetti, P., Brandt, N., Cavalleri, A., Ciani, G., Cristofolini, I., Cruise, A., & others. (2009). LISA Pathfinder: the experiment and the route to LISA. Classical and Quantum Gravity, 26(9), 094001.
    2. Böhm, C., Merk, M., Fichter, W., & Allgöwer, F. (2009). 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, 511–520.
    3. Grynagier, A., Fichter, W., & Vitale, S. (2009). The Drift Mode for LISA Pathfinder: Implementation Solutions for a Robust Algorithm. Classical and Quantum Gravity, 26(9), Article 9.
    4. Hewitson, M., Armano, M., Benedetti, M., Bogenstahl, J., Bortoluzzi, D., Bosetti, P., Brandt, N., Cavalleri, A., Ciani, G., Cristofolini, I., & others. (2009). Data analysis for the LISA Technology Package. Classical and Quantum Gravity, 26(9), 094003.
    5. Monsky, A., Hewitson, M., Ferraioli, L., Wanner, G., Nofrarias, M., Hueller, M., Diepholz, I., Grynagier, A., Armano, M., Benedetti, M., & others. (2009). The first mock data challenge for LISA Pathfinder. Classical and Quantum Gravity, 26(9), 094004.
  13. 2008

    1. Grimm, W., & Rotärmel, W. (2008). Integrated Guidance and Control for Entry Vehicles. From Nano to Space - Applied Mathematics Inspired by Roland Bulirsch.
  14. 2007

    1. Fichter, W., Schleicher, A., & Vitale, S. (2007). Drag-Free Control Design with Cubic Test Masses. Lasers, Clocks, and Drag-Free Control, 349(December), Article December.
  15. 2005

    1. Fichter, W., Gath, P., Vitale, S., & Bortoluzzi, D. (2005). LISA Pathfinder drag-free control and system implications. Classical and Quantum Gravity, 22(10), S139.
  16. 1994

    1. Jänsch, C., Schnepper, K., & Well, K. (1994). Multi-phase trajectory optimization methods with applications to hypersonic vehicles. In Applied Mathematics in Aerospace Science and Engineering (pp. 133--164). Springer.
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