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- W2306543240 abstract "The SHEFEX-2 rocket was successfully launched in June, 2012 from AndoyaRocket Range in Norway by the German Aerospace Center. The main purpose ofthis mission was to investigate possible new shapes for future launcher or re-entryvehicles, specifically, shapes with faceted surfaces and sharp edges. The rocketwas unguided during the propelled flight phases and actively controlled duringreentry with canards.The SHEFEX-3 mission is proposed to further pursue the technology developmentfor reentry vehicles using the extended flight experiment and shall belaunched in 2016 in a suborbital trajectory.The accurate control of the SHEFEX-3 vehicle using control flaps and movingmasses requires a high-accuracy measurement of the angle of attack and the sideslip angle. Both angles can only be derived from the flight path and an accurateinertial attitude measurement. The first can be achieved by using GPS measurements.The second can not be provided by an inertial navigation system due tothe fact that drifts resulting from launch vibrations exceed the tolerance of the system.Therefore, a star tracker and sun sensors are utilized to update the attitudeinformation shortly before re-entry. The presented work will describe the conceptof the integrated hybrid navigation system. A special focus is also placed on theanalysis of how the attitude sensors can be integrated into the SHEFEX-3 probe." @default.
- W2306543240 created "2016-06-24" @default.
- W2306543240 creator A5003739167 @default.
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- W2306543240 date "2013-08-14" @default.
- W2306543240 modified "2023-09-27" @default.
- W2306543240 title "DEVELOPMENT OF A HYBRID NAVIGATION SYSTEM FOR THETHIRD SHARP EDGE FLIGHT EXPERIMENT (SHEFEX-3)" @default.
- W2306543240 hasPublicationYear "2013" @default.
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