AIAA Infotech Aerospace Conference lt br gt and lt br gt AIAA Unmanned Unlimited Conference AIAA 2009 2033 6 9 April 2009 Seattle Washington Static Verification of Spacecraft Procedures Erin M Connors College of William and Mary Williamsburg VA USA Cesar A Munoz National Institute of Aerospace Hampton VA USA Cameron Schnur Stevens Institute of Technology Hoboken NJ USA Radu Siminiceanu National Institute of Aerospace Hampton VA USA The Automati
SSC99 XII 6 Spacecraft Computers on the SeaStar Satellite Sawat Tantiphanwadi Ph D Orbital Sciences Corporation 1521 Westbranch Dr McLean VA 22102 Phone 703 883 2600 ext 2314 Email tanti sawat orbital com Abstract The SeaStar spacecraft requires a high performance computer system to handle its various requirements It must process not only the high rate data from the Sea viewing Wide Field of view Sensor SeaWiFS instrument but also the spacecraft ground int
Methods for Analysis of Preliminary Spacecraft Designs AAE450 Spacecraft Design Purdue University Written by Steven P Schneider Professor Adapted from Methods Developed by W Gustafson Professor Emeritus School of Aeronautics and Astronautics Purdue University September 19 2005 Contents Introduction 2 List of Analysis Tools 3 Architecture of Framework Programs 4 Rough Summary of Interdisciplinary Dependencies 6 Structural Analysis and Center of Gravity Analysis 7
7S GAISLER RESEARCH Spacecraft Data Handling IP Core User s Manual Based on GRLIB Sandi Habinc Copyright Gaisler Research May 2008 Table of contents TAO GUC HOt os cca toaca Aa oala A da ta ad 6 1 1 O cm eee Aaa ea aie a Ae ae EN 6 1 2 Implementation characteristics anna nana aa nana nana ae anna 6 1 3 A NN 6 AHB2PP AMBA AHB to Packet Parallel Interface nenea nana 8 2 1 A A A A ase se Mizzi 8 2 2 RN 8 2 3 RE GQIStETS al nl ai dle 9 2 4 AHB W O
Battery Operations for the TET 1 Spacecraft Kay M ller and Arvind Kumar Balan Deutsches Zentrum f r Luft und Raumfahrt e V German Aerospace Center M nchener Stra e 20 82234 Wefling Germany The TET 1 satellite serves as a technology demonstrator within the On Orbit Verifi cation OOV program with the goal of providing German space companies and research institutions with the opportunity to test their equipment on actual spacecraft It was launched on July 22
Methods for Analysis of Preliminary Spacecraft Designs AAE450 Spacecraft Design Purdue University Written by Steven P Schneider Associate Professor Adapted from Methods Developed by W Gustafson Professor Emeritus School of Aeronautics and Astronautics Purdue University August 18 2003 Contents Introduction 2 List of Analysis Tools 3 Architecture of Framework Programs 4 Structural Analysis and Center of Gravity Analysis 6 Orbital Dynamics 6 5 1 Conversion Between R