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Autonomous Rendezvous: Guidance and Control in Elliptical Orbit

, , , , and . American Institute of Aeronautics and Astronautics, (August 2007)
DOI: 10.2514/6.2007-6355

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Autonomous Rendezvous: Guidance and Control in Elliptical Orbit, , , , and . American Institute of Aeronautics and Astronautics, (August 2007)Dynamics modeling and comparative robust stability analysis of a space launcher with constrained inputs., , , , and . ECC, page 353-358. IEEE, (2013)Worst Case Analysis of a Launcher Vehicle Using Surrogate Models., , , , , and . ROCOND, page 260-265. International Federation of Automatic Control, (2012)Evaluating Regions of Attraction of LTI Systems with Saturation in IQS Framework., , , and . ROCOND, page 242-247. International Federation of Automatic Control, (2012)PWM Modeling for Attitude Control of a Launcher During Ballistic Phase and Comparative Stability Analysis., , , , , , and . ROCOND, page 248-253. International Federation of Automatic Control, (2012)Robust Safety Margin Assessment and Constrained Worst-Case Analysis of a Launcher Vehicle., , , , , and . ROCOND, page 254-259. International Federation of Automatic Control, (2012)Measures and LMI for Space Launcher Robust Control Validation., , and . ROCOND, page 236-241. International Federation of Automatic Control, (2012)