Compressed polynomial approach for onboard ephemeris representation

Author:

Sheela B. V.1,Padmanabhan P.1

Affiliation:

1. Indian Space Research Organization Satellite Centre, Bangalore, India

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

Reference15 articles.

1. ^ielsen, J. N., Missile Aerodynamics, McGraw-Hill, New York, 1960.

2. 3Spreiter, J. R. "The Aerodynamic Forces on Slender Plane and Cruciform-Wing and Body Combinations," NACA Rept. 962,1950.

3. Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail Configuration

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