Spin Effect Correction Method for Spacecraft Orbit Measurement Data

A theoretical analysis is conducted to ranging and Doppler velocity measurement data ple. A correction method is proposed for rangin tion method can also estimate the alignment of ranging and Doppler velocity measurement data evaluate the effect of the spin of a spacecraft on from the perspective of the measurement princi- g and Doppler velocity measurement. The correc- the on-board antenna. In the processing of CE-2 during the earth-moon transfer phase, the error of the estimated alignment of the on-board antenna is approximately se bit determination is performed by using the corrected ranging and Doppler and the results show that the correction for the data can improve the orbital veral centimeters. The or- velocity measurement data, accuracy by 50m.