发明名称 |
Digital radar altimeter |
摘要 |
A method for determining a height above ground of an aircraft broadly comprises the steps of generating a transmit signal with a transmitter, transmitting the transmit signal with a first antenna, generating a local oscillator signal with a local oscillator, receiving a receive signal with a second antenna, mixing the receive signal with the local oscillator signal to generate a baseband signal, determining a frequency of interest of the baseband signal, and calculating an aircraft altitude corresponding to the frequency of interest. |
申请公布号 |
US9075144(B1) |
申请公布日期 |
2015.07.07 |
申请号 |
US201213660504 |
申请日期 |
2012.10.25 |
申请人 |
Garmin International, Inc. |
发明人 |
Straub Edward M.;Johnson John C.;Werling Heather M. |
分类号 |
G01S13/08;G01S13/88;G01S13/34 |
主分类号 |
G01S13/08 |
代理机构 |
|
代理人 |
Korte Samuel M.;Ali Mohammad M. |
主权项 |
1. A method for determining a height above ground of an aircraft, the method comprising the steps of:
generating, using a local oscillator linear sweep generator, a local oscillator signal that is swept over a frequency range; generating, using a transmitter linear sweep generator, a transmit signal with a transmitter that is swept over the frequency range and delayed in time with respect to the local oscillator signal; transmitting the transmit signal with a first antenna; receiving a receive signal with a second antenna; mixing, using a mixer, the receive signal with the local oscillator signal to generate a baseband signal having a frequency of interest for calculating an aircraft altitude; adjusting, using a controller, the delay in time while the aircraft is on the ground until the frequency of interest is at least equal to a minimum difference frequency; and calculating, using the controller, the aircraft altitude based on the frequency of interest determined from the receive signal and the local oscillator signal. |
地址 |
Olathe KS US |