4/7/13    08:30 - 11:50 FD.6: Launchers and Spacecrafts Guidance

ThM02 Room: Novotel Tegernsee Chair: Alexander V. Nebylov Rapporteur: to be confirmed

Guidance and control law for D-SEND#2. H. Suzuki , T. Ninomiya and J. Kawaguchi Adaptive Guidance Law for Trajectory Control of a Reusable Launch Vehicle during Air-Breathing Ascent Phase V. Brinda, K. Sivan and S. Dasgupta Ascent Trajectory Guidance for an Impulsive Orbit Injection (*) A.L. Nepomuceno Real-time impact control of a solid rocket motor stage during launcher ascent(*) L. Perrot and S. Hervouet Day-of-launch wind biasing trajectory optimization impact on launch vehicles pre-dimensioning methodologies D. Delorme, J. Desmariaux, B.  Carpentier and A. Espinosa Analtical techenquis in astrodynamics W. A Rahoma and F. Deleflie Robust Autonomous Aerobraking Strategies T. Chabot, G. Bonnéry, S. Val Serra, S. Kemble, H. Scheer, F. Forget, T. Voirin, S. Salehi and D. Gherardi