Terrain-Relative and Beacon-Relative Navigation for Lunar Powered Descent and Landing
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF03321162.pdf
Reference9 articles.
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2. WOFFINDEN, D.C. and GELLER, D.K. “Relative Angles-Only Navigation and Pose Estimation for Autonomous Orbital Rendezvous,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 5, Sept–Oct 2007, pp. 1455–1469.
3. LEFFERTS, E.J., MARKLEY, F.L., and SHUSTER, M. “Kalman Filtering for Spacecraft Estimation,” Journal of Guidance, Control, and Dynamics, Vol. 5, No. 5, 1982, pp. 417–429.
4. PITTELKAU, M.E. “Rotation Vector in Attitude Estimation,” Journal of Guidance, Control, and Dynamics, Vol. 26, No. 6, 2003, pp. 855–860.
5. CRASSIDIS, J.L. and JUNKINS, J.L. Optimal Estimation of Dynamic Systems, ch. 5, CRC Press, 2004, pp. 243–329.
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