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Ground clutter processing for wind measurements with airport surveillance radars
November 4, 1987
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-143
Summary
Modern airport surveillance radars (ASR) are coherent pulsed-Doppler radars used for detecting and tracking aircraft in terminal area air-space. These radars might serve an additional role by making radial wind measurements in the immediate vicinity of an airport to provide data on low altitude wind shear (LAWS). One factor that will affect their capability in this role is the requirement that intense low-beam ground clutter be filtered from the signals prior to estimation of the reflectivity and radial velocity of weather scatterers. This report describes and analyzes a specific signal processing algorithm for ASR weather parameter measurements. An adaptively selected Finite Impulse Repsonse high-pass filter is used for ground clutter suppression, followed by pulse-pair weather reflectivity and radial velocity estimation. Measurements from a Lincoln Laboratory-developed testbed ASR in Huntsville, Alabama are used to characterize the ground clutter environment under siting ocnditions that are representative of operational ASRs. Temporal fluctuations in ground clutter intensity are analyzed with attention to their impact on the adaptive clutter-filter selection procedure. The performance of the signal processing algorithms is then analyzed using the testbed ASR ground clutter measurements in combination with simulated or real weather signals. We conclude that ground clutter and hte requisite clutter filtering will not severely distort ASR wind shear measurements when the reflectivity factor of the microburst or gust front is approximately 20 dBz or greater. This is typically the case for microbursts ocurring in moist conditions such as prevail over the Eastern United States during summer.
Summary
Modern airport surveillance radars (ASR) are coherent pulsed-Doppler radars used for detecting and tracking aircraft in terminal area air-space. These radars might serve an additional role by making radial wind measurements in the immediate vicinity of an airport to provide data on low altitude wind shear (LAWS). One factor that...
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Surveillance processing in the Mode S sensor
October 21, 1987
Conference Paper
Published in:
Radar-87, IEE Int. Conf., London, U.K., 19-21 October 1987, pp. 189-194.
Summary
The principal function of the Mode S sensor (1), an evolutionary upgrade to the current ATCRBS (Air Traffic Control Radar Beacon System) sensor, is the output of one reportper aircraft per antenna scan. This report contains the current aircraft position (range and azimuth), the identity code of its transponder, and the altitude code as supplied by its encoding altimeter. This information is derived from the aircraft transponder replies received at the sensor in response to interrogations transmitted by the sensor. For aircraft equipped with Mode S transponders, a single scheduled interrogation, directed only to that aircraft, elicits a single coding-protected reply containing both identity code and altitude code. For aircraft equipped with ATCRSS transponders, a sequence of interrogations alternately eliclt replies containing un-protected identity code or altitude code from all aircraft in the antenna mainbeam. From this description, it is clear that a Mode S aircraft report can be constructed directly fron the single reply. Surveillance processing, defined as functions that perform scan-to-scan correlation and tracking, are required in general only to predict the next scan position of the aircraft. This information is needed for the proper scheduling of the next interrogation. ATCRBS reports constructed from the aircraft replies, on the other hand, can have a number of deficiencies. The more common such problems are: 1. Either the identity code or altitude code or both can have bits declared either in error or with low confidence by the reply processor due to garbling of overlapping replies. 2. False alarm reports not corresponding to aircraft can be generated from fruit replies (responses to other sensors' interrogations) or reflection replies. 3. Multiple reports for an aircraft can be generited due to incorrect correlation of replies caused by errors in range, azimutn, or code determination. Surveillance processing for ATCRBS aircraft is tasked with correcting these problems prior to report output to the controllers or other users. It does this by correlating raw target reports with, existing track files, and using the information in these files derived from prior scan reports to correct, complete, or reject erroneous reports. This paper presents the major algorithms contained within the Mode S sensor ATCRBS surveillance processing function. It then presents experimental results that demonstrate their effectiveness. Full details of surveillance processing can be obtained by reference to (2) or [3).
Summary
The principal function of the Mode S sensor (1), an evolutionary upgrade to the current ATCRBS (Air Traffic Control Radar Beacon System) sensor, is the output of one reportper aircraft per antenna scan. This report contains the current aircraft position (range and azimuth), the identity code of its transponder, and...
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Mode S beacon system: functional description (revision D)
August 29, 1986
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-42-D
Summary
This document provides a functional description of the Mode S Beacon System, a combined secondary surveillance radar (beacon) and ground-air-ground data link system capable of providing the aircraft surveillance and communications necessary to support ATC automation in future traffic environments. Mode S is capable of common-channel interoperation with the current ATC beacon system, and may be implemented at low user cost over an extended transition period. Mode S will provide the surveillance and communication performance required by the ATC automation, the reliable communications needed to support data link services, and the capability of operating with a terminal or enroute, radar digitizer-equipped, ATC surveillance radar. The material contained in this document updates and expands the information presented in "Mode S Beacon System: Functional Description", DOT/FAA/PM-83/8, 215 July 1983.
Summary
This document provides a functional description of the Mode S Beacon System, a combined secondary surveillance radar (beacon) and ground-air-ground data link system capable of providing the aircraft surveillance and communications necessary to support ATC automation in future traffic environments. Mode S is capable of common-channel interoperation with the current...
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Effect of interference on the performance of a minimum TCAS II
September 5, 1985
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-132
Summary
Minimum TCAS II equipment is required to operate reliably in all aircraft densities up to the 0.3 transponder-equipped aircraft per square nautical mile anticipated in the Los Angeles Basin in the year 2000. Prototype TCAS equipment has been developed and shown to be capable of providing reliable surveillance in today's highest densities, which reach an average of about 0.1 aircraft per square nmi. Since there are no existing environments that reach the density of asynchronous interference anticipated for the Los Angeles Basin in the year 2000, it is necessary to generate simulated interference to determine the performance of the TCAS II design in that environment. A series of bench tests were conducted at Lincoln Laboratory for this purpose. Special sources were used to generate asynchronous ATCRBS and Mode S reply signals (Fruit) and TCAN/DME squitter and interrogation signals. Synchronous ATCRBS and Mode S reply sequences were also generated to simulate airborne encounters. The performance was evaluated by observing hoe the interference signals either degraded the ability of a TCAS II unit to receive, process, and track the desired synchronous reply sequences, or caused the TCAS II unit to generate false tracks.
Summary
Minimum TCAS II equipment is required to operate reliably in all aircraft densities up to the 0.3 transponder-equipped aircraft per square nautical mile anticipated in the Los Angeles Basin in the year 2000. Prototype TCAS equipment has been developed and shown to be capable of providing reliable surveillance in today's...
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TCAS II ATCRBS surveillance algorithms
January 28, 1985
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-131
Summary
The Traffic Alert and Collision Avoidance System (TCAS) has been developed to reduce mid air collisions between transponder equipped aircraft. The TCAS concept encompasses a range of capabilities. TCAS I is a low-cost version which provides traffic advisories only. TCAS II adds vertical resolution advisories and is intended to provide a comprehensive level of separation assurance in all current and predicted airspace environments through the end of this century. Enhanced TCAS II uses more accurate intruder bearing data to allow it to generate horizontal resolution advisories. All three forms of TCAS equipment track aircraft equipped with both the existing Air Traffic Control Radar Beacon System (ATCRBS) transponders and with the new Mode S transponders. A TCAS equipped aircraft makes ATCRBS or Mode S range measurements on nearby aircraft. The ATCRBS or Mode S replies contain the altitude of the aircraft if it has an encoding altimeter. TCAS II uses range rate and altitude rate to decide if a collision is imminent. Therefore the replies from a given aircraft must be tracked and correlated in range and altitude. This report documents surveillance techniques developed by Lincoln Laboratory for use by TCAS II equipment in tracking aircraft equipped with ATCRBS transponders. Specifically, it describes the two tracking algorithms used for ATCRBS replies. One algorithm is for aircraft that report altitude, and the other is for those that do not.
Summary
The Traffic Alert and Collision Avoidance System (TCAS) has been developed to reduce mid air collisions between transponder equipped aircraft. The TCAS concept encompasses a range of capabilities. TCAS I is a low-cost version which provides traffic advisories only. TCAS II adds vertical resolution advisories and is intended to provide...
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A high stability TWTA for ground surveillance applications
March 13, 1984
Conference Paper
Published in:
Proc. 1984 IEEE Natl. Radar Conf., 13-14 March 1984, pp. 110-114.
Summary
A high stability, C-band transmitter capable of supporting -68 dBr subclutter visibility over a wide range of pulse widths and duty factors was developed for use in a multimode, battlefield surveillance radar. The transmitter was mode-switched between groups of 1/4, 20 and 65 microsecond radar pulses and long duration (100ms) FSK burst. A key feature was the use of a high speed, interpulse regulator to maintain proper TWT voltage and to limit ripple independent of waveform without the need for excessively large energy storage. Actual measured performance met the 100 mV cathode ripple specification without the use of PKF synchronization, independent of PKI, duty cycle and pulse width and was confirmed via direct evaluation of electrode voltages, serrodyne phase jitter and the radar pulsed-Doppler spectrum.
Summary
A high stability, C-band transmitter capable of supporting -68 dBr subclutter visibility over a wide range of pulse widths and duty factors was developed for use in a multimode, battlefield surveillance radar. The transmitter was mode-switched between groups of 1/4, 20 and 65 microsecond radar pulses and long duration (100ms)...
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Development of surveillance techniques for TCAS II
March 5, 1984
Conference Paper
Published in:
IEE Colloquium on Airborne Collision Avoidance, London, Uk, 5 March 1984, PP. 2/1-2/4.
Summary
In the development program of airborne collision avoidance, the equipment intended for installation on air carriers is designated TCAS 11 in the United States. A TCAS 11 installation my be thought of as consisting of two major subsystems: (1) air-to-air surveillance, and (2) control logic (including the logical tests that decide when another aircraft is dangerously close, algorithm that select an appropriate vertical resolution advisory, and a display of the advisory to the pilot). This paper focuses on the air-to-air surveillance subsystem. It identifies the disturbance phenomena that affect performance, presents a number of techniques that have been developed to overcome these difficulties, and presents performance measurements made through airborne testing. A TCAS II installation carries out surveillance in both Mode S and Mode C. The former is used for all Mode S aircraft, including other TCAS II aircraft. The latter is used for all other aircraft, provided they are equipped to reply in Mode C. This paper concentrates on surveillance in Mode C, which is by far the more demanding case.
Summary
In the development program of airborne collision avoidance, the equipment intended for installation on air carriers is designated TCAS 11 in the United States. A TCAS 11 installation my be thought of as consisting of two major subsystems: (1) air-to-air surveillance, and (2) control logic (including the logical tests that...
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Mode S Beacon System: Functional Description (Revision C)
July 15, 1983
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-42,C
Summary
This document provides a functional description of the Mode S Beacon Systme, a combined secondary surveillance radar (beacon) and ground-air-ground data link system capable of providing the aircraft surveillance and communications necessary to support ATC automation in future traffic environments. Mode S is capable of common-channel interoperation with the current ATC beacon system, and may be implemented at low user cost over an extended transition period. Mode S will provide the surveillance and communication performance required by the ATC automation, the reliable communications needed to support data link services, and the capability of operating with a terminal or enroute, radar digitizer-equipped, ATC surveillance radar. The material contained in this document updates and expands the information presented in "Mode S Beacon System: Functional Description", DOT/FAA/RD-82/52, 27 October 1982.
Summary
This document provides a functional description of the Mode S Beacon Systme, a combined secondary surveillance radar (beacon) and ground-air-ground data link system capable of providing the aircraft surveillance and communications necessary to support ATC automation in future traffic environments. Mode S is capable of common-channel interoperation with the current...
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Traffic Alert and Collision Avoidance System (TCAS): a functional overview of active TCAS I
April 8, 1983
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-118
Summary
The Traffic Alert and Collision Avoidance System (TCAS) is a beacon-based airborne collision avoidance system that is able to operate in all airspace without reliance on ground equipment. The TCAS concept encompasses a range of capabilities that include TCAS I, a low-cost, limited-performance version, and TCAS II, which is intended to provide a comprehensive level of separation assurance in all current and predicted airspace enviornments through the end of this century. This document provides a functional overview of a TCAS I equipped with a low power active transponder detector. It includes a definition of TCAS I functions, calculated and measured surveillance performance for a low power interrogator and an implementation approach that incorporates the TCAS I functions in a Mode S transponder.
Summary
The Traffic Alert and Collision Avoidance System (TCAS) is a beacon-based airborne collision avoidance system that is able to operate in all airspace without reliance on ground equipment. The TCAS concept encompasses a range of capabilities that include TCAS I, a low-cost, limited-performance version, and TCAS II, which is intended...
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Generation of the mode select sensor network coverage map
November 24, 1982
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-98A
Summary
This paper describes the technique of desiging the network management coverage map files necessary to coordinate a network of Mode S sensors. First, the concept of the Mode S network is defined, and the functions of Network Management are briefly described, as they relate to the coverage map. Then, the rationale for the coverage map is given together with definitions of the map structure and the information required in the file. Implementation of these definitions is illustrated in terms of a specific example: a network of four Mode S sensors in the Washington, D.C. area. As configured, each of the sensors provides service to only one of four ATC facilities (three TRACONs and one ARTCC). The resulting map generation process illustrates not only the general principles but also the significant effects of the ATC control are geometry. Finally, the procedure requored for automated map generation is defined. This procedure assumes the use of an interactive computer display terminal and is applicable to any sensor network and ATC facility configuration.
Summary
This paper describes the technique of desiging the network management coverage map files necessary to coordinate a network of Mode S sensors. First, the concept of the Mode S network is defined, and the functions of Network Management are briefly described, as they relate to the coverage map. Then, the...
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