Blazing Gyros: The Evolution of Strapdown Inertial Navigation Technology for Aircraft-Reference-Cited by-同舟云学术

Blazing Gyros: The Evolution of Strapdown Inertial Navigation Technology for Aircraft

Published:2013-05 Issue:3 Volume:36 Page:637-655
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Savage Paul G.¹

Affiliation:

1. Strapdown Associates, Inc., Maple Plain, Minnesota 55359

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.60211

Reference42 articles.

1. MacKenzieD., Inventing Accuracy, MIT Press, Cambridge, MA, 1993, pp. 71–92, Chap. 2.

2. EberleinA. J.SavageP. G. “Strapdown Cost Trend Study and Forecast,” NASA Ames Research Center CR-137585, 1 Jan. 1975.

3. GilmoreJ. P. “Non-Orthogonal Gyro Configuration,” Massachusetts Inst. of Technology/Instrumentation Laboratory Rept. T-472, Jan. 1967.

4. GilmoreJ. P.CooperR. J. “SIRU Development–Final Report, Volume 1, System Development,” Draper Lab., NASA CSDL-R-746, CR-136033, 1973.

5. HrubyR. J.BjorkmanW. S. “Flight Test Results of the Strapdown Hexad Inertial Reference Unit (SIRU),” NASA Ames Research Center TMX-73,223, July 1977.

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