Noniterative Instantaneous Impact Point Prediction Algorithm for Launch Operations
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
2. Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea
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/10.2514/1.56395
Reference16 articles.
1. GPS based prediction of the instantaneous impact point for sounding rockets
2. Regan, F., and Anandakrishnan, S. M., Dynamics of Atmospheric Re-Entry, AIAA Education Series, AIAA, Washington, D.C., 1984, pp.145-161.
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