| 摘要 |
<p>An aircraft altimeter has a planar transmit antenna 2 and receive antenna 3 on the same substrate separated by about 150mm. An oscillator 20 supplies microwave energy in the G-band to the transmit antenna via a pulse modulated amplifier 21. The oscillator also supplies an output via a phase shifter 23 to one input of a mixer 24 the other input of which is supplied with the received signals from the receive antenna 3. The phase shifter 23 is controlled to adjust the phase of the signal supplied to the mixer 24 from the oscillator 20 so that it cancels out the leakage signal caused by direct coupling between the transmit and receive antennas 2 and 3. <IMAGE></p> |
