Three-Axis Attitude Determination Using Global Positioning System Signal Strength Measurements-Reference-Cited by-同舟云学术

Three-Axis Attitude Determination Using Global Positioning System Signal Strength Measurements

Published:2003-03 Issue:2 Volume:26 Page:304-310
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lightsey E. Glenn¹,Madsen Jared¹

Affiliation:

1. University of Texas at Austin, Austin, Texas 78712-1085

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/10.2514/2.5047

Reference17 articles.

1. 1Lightsey, E. G. “Development and Flight Demonstration of a GPS Receiver for Space,” Ph.D. Dissertation,Dept. Aeronautics and Astronautics, Stanford Univ., Stanford, CA,Feb. 1997.

2. Spacecraft attitude estimation using the Global Positioning System - Methodology and results for RADCAL

3. 5Ward, L. M. “Spacecraft Attitude Estimation Using GPS: Methodology and Results,” Ph.D. Dissertation,Dept. Aerospace Engineering Science, Univ., Colorado, Boulder, CO,Aug. 1996.

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