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An altimetry system for a satellite, including an altimeter transmitting and receiving signals on at least one first frequency band; a radiometer receiving signals on at least one second frequency band, the altimeter and the radiometer being connected to one and the same antenna; reception means com

An altimetry system for a satellite, including an altimeter transmitting and receiving signals on at least one first frequency band; a radiometer receiving signals on at least one second frequency band, the altimeter and the radiometer being connected to one and the same antenna; reception means common to the altimeter and to the radiometer, and capable of amplifying and filtering the signals received from the antenna on a frequency band including the first frequency band and the second frequency band; means for separating the signals on the first frequency band from the signals on the second frequency band; the signals on the first frequency band being exploited to estimate an altimetric distance of the satellite, and radiometric measurements being exploited in order to correct the estimate.

대표청구항 ▼

1. An altimetry system comprising: an altimeter transmitting and receiving signals on at least one first frequency band;a radiometer receiving signals on at least one second frequency band;an antenna connected to the altimeter and the radiometer;reception means common to the altimeter and to the rad

1. An altimetry system comprising: an altimeter transmitting and receiving signals on at least one first frequency band;a radiometer receiving signals on at least one second frequency band;an antenna connected to the altimeter and the radiometer;reception means common to the altimeter and to the radiometer, and capable of amplifying and filtering the signals received from the antenna on a frequency band comprising the first frequency band and the second frequency band;separation means for separating the signals on the first frequency band from the signals on the second frequency band; anda digital processing unit configured to exploit the signals on the first frequency band to generate an estimate of an altimetric distance of the satellite, andconfigured to exploit radiometric measurements of the second frequency band to correct the estimate,wherein the altimeter, the radiometer, the antenna, the reception means and the separation means are installed on board a satellite. 2. The altimetry system according to claim 1, wherein the reception means comprise a low noise amplifier operating on a frequency band comprising the said first frequency band and the said second frequency band. 3. The altimetry system according to claim 1, wherein the reception means comprise a band-pass filter capable of selecting a frequency band comprising the said first frequency band and the said second frequency band. 4. The altimetry system according to claim 3, further comprising interconnection means for connecting the altimeter and the radiometer to the antenna and for isolating the transmission and reception channels, the interconnection means comprising a first circulator including a first port connected to the antenna, a second port connected to a switch connected to a transmission channel of the altimeter, and a third port connected to a switch connected to the reception means common to the altimeter and to the radiometer. 5. The altimetry system according to claim 4, wherein the reception means are connected to a first circulator connected via a first port to the interconnection means, and connected via a second port to calibration means for calibrating the radiometer, the calibration means comprising a hot source and a cold source configured to be connected alternately to the first circulator. 6. The altimetry system according to claim 1, wherein the signal-separation means comprise a rejection filter for rejecting the first frequency band, from the signals amplified and filtered by the reception means. 7. The altimetry system according to claim 1, wherein the first frequency band and the said second frequency band are included in the Ka band. 8. The altimetry system according to claim 1, wherein a minimum boundary of the second frequency band coincides with a maximum boundary of the first frequency band, or a maximum boundary of the second frequency band coincides with a minimum boundary of the first frequency band. 9. An altimetric payload for a satellite comprising: a device for positioning the satellite relative to an Earth reference point; andan altimetry system comprising: an altimeter transmitting and receiving signals on at least one first frequency band,a radiometer receiving signals on at least one second frequency band,an antenna connected to the altimeter and the radiometer,reception means common to the altimeter and to the radiometer and configured to perform amplifying and filtering the signals received from the antenna on a frequency band including the first frequency band and the second frequency band, andseparation means for separating the signals on the first frequency band from the signals on the second frequency band. 10. A method of altimetric measurement from a satellite, the method comprising a step of transmitting a signal from said satellite to the Earth's surface;a step of calibrating a radiometer carried by said satellite, said step of calibrating being performed during time intervals not used for transmitting said signal or during waiting for an echo originating from a reflection of said signal from the Earth's surface;a step of receiving, at the satellite, the echo;a step of concomitantly taking radiometric measurements using said radiometer;a step of processing said echo to generate an estimate of an altimetric distance of the satellite from the Earth's surface; anda step of correcting the estimate by exploiting said radiometric measurements, wherein at least some of said radiometric measurements are taken using a reception channel that is common to a reception channel for receiving the echo.