A Kalman-Filter Based Inertial Navigation System Processor for the SCRAMSPACE 1 Hypersonic Flight Experiment-Reference-Cited by-同舟云学术

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A Kalman-Filter Based Inertial Navigation System Processor for the SCRAMSPACE 1 Hypersonic Flight Experiment

Published:2012-09-24 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Creagh Michael¹,Beasley Peter²,Dimitrijevic Igor¹,Brown Melrose¹,Tirtey Sandy¹

Affiliation:

1. University of Queensland

2. CB Aerospace

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5894

Reference14 articles.

1. 1McClinton,C.R.,V.L.Rausch,etal.(2005)."PreliminaryX-43FlightTestResults."ActaAstronauticaVol.57(Issues 2-8):266-276.

2. Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment

3. 3Tahir, R.B., Mölder, S. and Timofeev, E.V. "UnsteadyStarting of High Mach Number Air Inlets - A CFD Study", AIAA-2003-5191,39thAIAA/ASME/SAE/ASEEJointPropulsionConference&Exhibit,Huntsville,AL,Jul2003.

4. 4Grainger, A.L., TirteyS.C., Boyce, R.R., Paris.S., andPaniagua,G. "StartingMechanisms for High Contraction Ratio HypersonicInlets,"In:Proceedings of7thESAAerothermodynamicsSymposium,Bruge,Belgium,May2011.

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