The present invention provides a whole arc section
satellite remote-control Doppler compensation method by calculating
satellite orbit and using DDS to realize the compensation, wherein, the
satellite orbits calculation method comprises that input data of earth
station location coordinates (
latitude,
longitude and height), satellite transient Keplerian
orbit 6
root number including major semi-axis, eccentricity, obliquity,
right ascension of the ascending node and mean anomaly, and time point, earth
station remote-control time period and
time step, and remote-
control signal carrier frequency, are used for performing geometry calculation to obtain accurate
orbit location of the satellite within the remote-control time period, furthermore, a
Doppler frequency bias value, a
Doppler frequency first-order change rate and a
Doppler frequency second-order change rate are obtained. The calculated Doppler corresponding data are transmitted to the DDS module to generate a frequency with a sign opposite to that of the Doppler frequency bias value and a same absolute value for modulating remote-control signals and generating Doppler frequency bias compensation. According to the present invention, after receiving remote-control signals, the satellite can realize capture of remote-
control signal carriers by using a smaller phase-lock
loop bandwidth, therefore,
carrier capture time is shortened,
carrier capture capability is improved, and interference to useful signals from the
noise in the
loop bandwidth is reduced.