The invention provides a navigation
constellation inter-
satellite link
transceiver device time
delay calibration method. The method comprises the steps of adding a bidirectional calibration channel, a medium-frequency
switch matrix and a radio-frequency
switch matrix on a
transceiver device, conducting time-sharing control on the radio-frequency
switch matrix and the medium-frequency switch matrix, sequentially enabling every two of a transmitting channel, a receiving channel and the bidirectional calibration channel to be communicated, performing
closed loop time
delay testing to obtain three time
delay values, and finally calculating an absolute time delay Tt of the transmitting channel and an absolute time delay Tr of the receiving channel according to the three time delay values, wherein the time delay amount serves as a
transceiver device time delay zero value to be substituted into inter-
satellite link time delay measurement data for time delay calibration, and transceiver device time delay calibration is achieved. By means of the navigation
constellation inter-
satellite link transceiver device time delay calibration method, on-
orbit real-time measurement of a transceiver can be achieved, and transceiver device delay calibration can be completed in a single satellite, namely the defect of
static testing is avoided. In addition, compared with other dynamic methods, multi-satellite or multi-antenna participated time delay measurement work is not needed.