VOR radiated VHF energy modulated with Reference signal (omni directional flash) and Variable phase signal (rotating beam) and the bearing of the VOR station is the phase difference between reference and variable phases (time difference between flash and beam).
The principle of VOR navigation involves a comparison of phase difference between the two transmitted signals.One of the signals is termed as the reference signal and the other one is variable signal.The use of AM and FM with a wide frequency separation between them prevents cross modulation between the signals which would otherwise cause bearing errors in the system.VOR transmitter radiates both unidirectional and omni directional signals.
The transmitter is crystal controlled and is amplitude modulated by A 30 Hz AM referred to as variable phase signal (directional signal) and A sub carrier AM of 9960 Hz with a deviation of plus minus 480 Hz which is frequency modulated at 30 Hz. (omni directional signal).A 1020 Hz AM is also transmitted for the station identification(morse code of 2 or 3 letters).The VOR beacon transmits a signal in all directions (omni directional).We call these signals “Radials”.The transmitted radials contain different information to separate the radials from each other.The VOR beacon radiates the first radial in the direction of magnetic north of the station (called zero radial).
The radial is measured from the difference in phase between the reference and variable signal.The 30 Hz reference signal always has the same phase whatever aircraft’s position with respect to the station.The phase of the variable signal varies with the aircraft’s position.VOR receiver receives the ground signal, detects and separates the phase and compares the phase of the two signals. The receiver is able to gives the magnetic and relative bearing of the transmitter,Deviation of the aircraft from a selected course andTo-From information.
VOR radiated VHF energy modulated with Reference signal (omni directional flash) and Variable phase signal (rotating beam) and the bearing of the VOR station is the phase difference between reference and variable phases (time difference between flash and beam).
The principle of VOR navigation involves a comparison of phase difference between the two transmitted signals.One of the signals is termed as the reference signal and the other one is variable signal.The use of AM and FM with a wide frequency separation between them prevents cross modulation between the signals which would otherwise cause bearing errors in the system.VOR transmitter radiates both unidirectional and omni directional signals.
The transmitter is crystal controlled and is amplitude modulated by A 30 Hz AM referred to as variable phase signal (directional signal) and A sub carrier AM of 9960 Hz with a deviation of plus minus 480 Hz which is frequency modulated at 30 Hz. (omni directional signal).A 1020 Hz AM is also transmitted for the station identification(morse code of 2 or 3 letters).The VOR beacon transmits a signal in all directions (omni directional).We call these signals “Radials”.The transmitted radials contain different information to separate the radials from each other.The VOR beacon radiates the first radial in the direction of magnetic north of the station (called zero radial).
The radial is measured from the difference in phase between the reference and variable signal.The 30 Hz reference signal always has the same phase whatever aircraft’s position with respect to the station.The phase of the variable signal varies with the aircraft’s position.VOR receiver receives the ground signal, detects and separates the phase and compares the phase of the two signals. The receiver is able to gives the magnetic and relative bearing of the transmitter,Deviation of the aircraft from a selected course andTo-From information.
Thank you for this wonderful information ! May the God almighty Bless You for this worked.
ReplyDeleteThis comment has been removed by the author.
ReplyDeleteclear and plain explanation. hank you
ReplyDelete