Method of correcting measurement errors caused by clock deviations in a secondary radar system
First Claim
1. A secondary radar system for Mode S operation, comprising:
- a plurality of ground stations, each ground station including a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of reply signals;
a plurality of antennas respectively connected to said interrogators;
at least one airborne station that transmits a reply signal in response to a received interrogation signal;
measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a reply signal;
synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame;
said measuring means, including computing means for computing a signal transmit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return; and
means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame;
the further reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators.
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Accused Products
Abstract
Conventional secondary radar systems use mechanically rotating antennas to radiate a concentrated beam that rotates in a horizontal plane. Data exchange between ground stations and airborne transponders can only take place if the aircraft is struck by the antenna lobe. The distance from the aircraft to the ground station is determined from the signal transit time. Directional information is derived from the antenna position. The secondary radar system according to the invention uses an omnidirectional antenna, so that data can be exchanged between ground station and aircraft at any time. To determine the position of the aircraft, interrogation signals are transmitted by a single active ground station such that the reply signal from a transponder falls within the common system time frame of the ground station. The times of arrival of the reply signals at different ground stations are then directly proportional to the distances from the aircraft to these ground stations.
Measurement errors caused by clock deviations are corrected by determining any deviation of the clocks of two ground stations from each other. To correct clock deviations, two interrogation/reply cycles are used in direct succession in opposite directions over a common transmission path. The two transmission periods will differ by twice the deviation of the clocks in the two ground stations. The measured deviation is used to correct the measured transit time values and/or to synchronize the clocks. Synchronization of several ground stations with a master station can be achieved by using successive interrogation/reply cycles between the master station and all other stations.
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Citations
23 Claims
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1. A secondary radar system for Mode S operation, comprising:
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a plurality of ground stations, each ground station including a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of reply signals; a plurality of antennas respectively connected to said interrogators; at least one airborne station that transmits a reply signal in response to a received interrogation signal; measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a reply signal; synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame; said measuring means, including computing means for computing a signal transmit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return; and means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame; the further reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. In a secondary radar system for Mode S operation, having:
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a plurality of ground stations, each ground station including a clock and a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of first reply signals; a plurality of antennas respectively connected to said interrogators; at least one airborne station that transmits a first reply signal in response to a received interrogation signal; measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a first reply signal; synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame; said measuring means including computing means for computing a signal transit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return; and means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further first reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame; the further first reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators; a method of correcting measurement errors caused by clock deviations in the plurality of ground stations, comprising the steps of; transmitting toward said at least one airborne station from all the ground stations (S1-S4) which are used to determine a position of the at least one airborne station, a plurality of transmit interrogation signals in a cyclic sequence and at fixed points in time within another time frame that is predetermined by the clock of one of said plurality of ground stations (S1); receiving second reply signals from said at least one airborne station at all said ground stations, said second reply signals being responsive to said plurality of transmit interrogation signals; determining at each ground station receiving said second reply signals, a time of reception of said second reply signals; forming said plurality of ground stations into different respective pairs of ground stations; each of said different respective pairs of ground stations comprising one of said ground stations and one of a master ground station and another one of said ground stations; exchanging data between the ground stations of a selected pair of ground stations, said exchanged data representing an elapsed time that is calculated between a transmission of a transmit interrogation signal by one of said selected pair of ground stations and a reception by the other one of said selected pairs of ground stations of a second reply signal from said airborne station that is responsive to said transmit interrogation signal transmitted by said one of said selected pair of ground stations; calculating a first elapsed time for said selected pair of ground stations beginning at a first time when said one ground station of said selected pair of ground stations transmits a first transmit interrogation signal and ending at a second time when the other one of said selected pair of ground stations receives a second reply signal responsive to the first transmit interrogation signal transmitted by said one ground station; calculating a second elapsed beginning at another first time when said other one of said ground stations of said selected pair of ground stations transmits a second transmit interrogation signal and ending when the one ground station of said selected pair of ground stations receives another second reply signal from said airborne station that is responsive to said second transmit interrogation signal transmitted from said other ground station; and
whereinone-half of an absolute value of a difference between the first and second calculated elapsed times is representative of a deviation between the clocks of the ground stations of said selected pair of ground stations; and
thenadjusting a determination of a position of said at least one airborne station based on said deviation between said clocks. - View Dependent Claims (14, 15, 16, 17, 18, 19, 20)
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21. A secondary radar system for Mode S operation, comprising:
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a plurality of ground stations, each ground station including a clock and a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of first reply signals; a plurality of antennas respectively connected to said interrogators; at least one airborne station that transmits a first reply signal in response to a received interrogation signal; measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a first reply signal; synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame; said measuring means including computing means for computing a signal transit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return; means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further first reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame; the further first reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators; and correcting means for correcting pairs of clocks of said ground stations, said correcting means including; deviation determining means for determining any deviation between the clocks of selected pairs of said ground stations; and means for correcting a determination of a position of said at least one airborne station based on the deviation determined by said deviation determining means. - View Dependent Claims (22, 23)
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Specification