Orbit covariance inner integrals with polynomials

This paper describes the calculation, for permanent storage, of the inner integral II polynomials used in real-time calculation of the gravity orbit error covariance function QF (ifc+i, tk)- Inner integral applications to JASON-EGM96, Lunar Prospector - Lunar Prospector, and JASON-GRACE orbit-potential combinations are addressed, and graphical polynomial results are presented.