NASA NTRS · 19780018224
Long range orbital error estimation for applications satellites
Abstract
A method of optimum orbital averaging was employed to study the long range accuracy potential of polar orbiting applications satellites. This approach involved the determination of the boundary conditions of one set of differential equations of motion by adjusting the initial conditions in a least square sense with the use of data generated by another set of differential equations of motion.
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Bonavito, N. L., Foreman, J. C.. 1978-01-01. Long range orbital error estimation for applications satellites. https://ntrs.nasa.gov/citations/19780018224
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