Publications
Time-scale modification with inconsistent constraints
October 15, 1995
Conference Paper
Published in:
Proc. 1995 Workshop on Applications of Signal Processing to Audio Acoustics, 15-18 October 1995.
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Summary
A set theoretic estimation approach is introduced for timescale modification of complex acoustic signals. The method determines a signal that meets, in a least-squared error sense, desired temporal and spectral envelope constraints that are inconsistent. These constraints are generalized within the set theoretic framework to include other signal characteristics such as instantaneous frequency and group delay. The approach can enhance acoustic signals consisting of closely-spaced sequential time components, and is applicable to biological, underwater, and music sound processing.
Summary
A set theoretic estimation approach is introduced for timescale modification of complex acoustic signals. The method determines a signal that meets, in a least-squared error sense, desired temporal and spectral envelope constraints that are inconsistent. These constraints are generalized within the set theoretic framework to include other signal characteristics such...
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GPS-squitter automatic dependent surveillance broadcast: flight testing in the Gulf of Mexico
October 13, 1995
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-235
Summary
During November - December 1994, MIT Lincoln Laboratory conducted a field evaluation of the air surveillance capabilities of GPS-Squitter in the Gulf of Mexico. Three squitter ground stations were located in the vincinity of Morgan City, Louisiana, for this evaluation: two were located on offshore oil platforms, and the third was located at an onshore heliport. Surveillance coverage tests were flown over the Gulf with three test aircraft - two helicopters and one Cessna 421 fixed wing aircraft. The helicopters flew at altitudes ranging from 100 to 2000 feet above sea level and the Cessna flew at 7500 and 20,000 feet. Extended squitter messages broadcast by each of the test aircraft provided aircraft position and identification. This report documents results of these texts and compares measured coverage to predicted coverage from the ground stations. Based on the good agreement between predicted and measured performance, a description of a possible operational system is included that would provide surveillance of the entire Gulf region serviced by oil platform helicopters. The report concludes that GPS Squitter is a near-term option for providing accurate, real time surveillance of aircraft operating in the offshore airspace in the Gulf of Mexico.
Summary
During November - December 1994, MIT Lincoln Laboratory conducted a field evaluation of the air surveillance capabilities of GPS-Squitter in the Gulf of Mexico. Three squitter ground stations were located in the vincinity of Morgan City, Louisiana, for this evaluation: two were located on offshore oil platforms, and the third...
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Runway status light system demonstration at Logan Airport
October 12, 1995
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-206
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Summary
The Runway Status Light System (RSLS), developed under the FAA's Airport Surface Traffic Automation (ASTA) program, is intended to help reduce the incidence of runway incursions and airport surface accidents. It will do so by providing a preventive, back-up system of automatically controlled lights on the airport surface that inform pilots when runways are unsafe for entry or takeoff, and by providing controllers with enhanced surface radar displays. This report documents a proof-of-concept evaluation of the RSLS at Boston's Logan Airport. It details the methods used to provide the necessary surface surveillance and safety logic to allow a computer to operate the runway status lights and associated controller displays without human assistance. The system was installed and tested off-line at Boston's Logan Airport using an inexpensive commercial marine radar as a primary surveillance source. The system operated live and in real time but the runway status lights were not physically installed. They were displayed on a scale model of Logan Airport located in a demonstration room that had a good view of the airport. This allowed visual comparison between the actual aircraft and the resulting lights and displays. In addition to providing a convincing demonstration of the system, real-timing viewing of the aircraft movement was an important aid in the development of the surveillance processing and safety logic software. Surveillance performance and runway status light operational performance were evaluated quantitatively. The probability of tracking an aircraft in movement areas with line-of-sight coverage was better than 98%. The false track rate was about four per hour, and the surveillance jitter was about 1 meter rms. From an operational point of view, had there been real lights on the field, it appears that they would have provided the intended safety back-up with little impact on airport capacity or controller and pilot workload, Only once in 15 minutes would the pilot population have observed a light in an incorrect state for more than four seconds. From the point of view of a specific cockpit crew, only once in 36 operations would a runway status light have been seen in an incorrect state for more than four seconds, and, furthermore, only once in 50 operations would light illuminations have interfered with normal, safe traffic flow. These are encouraging results for a system in an early demonstration phase because significant improvement is possible in all of these performance measures. Specific suggestions for improvement are included in this document.
Summary
The Runway Status Light System (RSLS), developed under the FAA's Airport Surface Traffic Automation (ASTA) program, is intended to help reduce the incidence of runway incursions and airport surface accidents. It will do so by providing a preventive, back-up system of automatically controlled lights on the airport surface that inform...
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The ASR-9 Processor Augmentation Card (9-PAC)
October 2, 1995
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-232
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Summary
Since 1990, the Airport Surveillance Radar-9 (ASR-9) has been commissioned and installed at more than 60 of the largest airports in the United States, and future installations are planned at more than 60 additional airports. After the first several systems were put into daily operation, air traffic controllers began to lodge complaints about the radar's performance. Problems included the detection of "phantom" aircraft caused by the reflection of beacon interrogation signals off buildings and other aircraft, the radar's losing track of targets during parallel approaches and departures, the inability to track highly maneuverable military aircraft through high-G turns, radar clutter caused by highways and weather, and system overloading as a result of signal returns from flocks of migrating birds. An initial investigation of the sources of these problems focused on the radar's post-processor. Nearly all of the problems could be addressed by additions to the post-processor software, but the post-processor was already running near capacity and there was no means for expansion. Thus, a new processor - the ASR-9 Processor Augmentation Card (9-PAC) - was designed to augment the existing system to allow for a significant increase in processing power. New algorithms were developed to run in 9-PAC to address the problems cited by the controllers.
Summary
Since 1990, the Airport Surveillance Radar-9 (ASR-9) has been commissioned and installed at more than 60 of the largest airports in the United States, and future installations are planned at more than 60 additional airports. After the first several systems were put into daily operation, air traffic controllers began to...
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Military and government applications of human-machine communication by voice
October 1, 1995
Conference Paper
Published in:
Proc. Natl. Acad. Sci., Vol. 92, October 1995, pp. 10011-10016.
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Summary
This paper describes a range of opportunities for military and government applications of human-machine communication by voice, based on visits and contacts with numerous user organizations in the United States. The applications include some that appear to be feasible by careful integration of current state-of-the-art technology and others that will require a varying mix of advances in speech technology and in integration of the technology into applications environments. Applications that are described include (1) speech recognition and synthesis for mobile command and control; (2) speech processing for a portable multifunction soldier's computer; (3) speech- and language-based technology for naval combat team tactical training; (4) speech technology for command and control on a carrier flight deck; (5) control of auxiliary systems, and alert and warning generation, in fighter aircraft and helicopters; and (6) voice check-in, report entry, and communication for law enforcement agents or special forces. A phased approach for transfer of the technology into applications is advocated, where integration of applications systems is pursued in parallel with advanced research to meet future needs.
Summary
This paper describes a range of opportunities for military and government applications of human-machine communication by voice, based on visits and contacts with numerous user organizations in the United States. The applications include some that appear to be feasible by careful integration of current state-of-the-art technology and others that will...
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Sine-wave amplitude coding using a mixed LSF/PARCOR representation
September 20, 1995
Conference Paper
Published in:
Proc. 1995 IEEE Workshop on Speech Coding for Telecommunications, 20-22 Spetember 1995, pp. 77-8.
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Summary
An all-pole model of the speech spectral envelope is used to code the sine-wave amplitudes in the Sinusoidal Transform Coder. While line spectral frequencies (LSFs) are currently used to represent this all-pole model, it is shown that a mixture of line spectral frequencies and partial correlation (PARCOR) coefficients can be used to reduce complexity without a loss in quantization efficiency. Objective and subjective measures demonstrate that speech quality is maintained. In addition, the use of split vector quantization is shown to substantially reduce the number of bits needed to code the all-pole model.
Summary
An all-pole model of the speech spectral envelope is used to code the sine-wave amplitudes in the Sinusoidal Transform Coder. While line spectral frequencies (LSFs) are currently used to represent this all-pole model, it is shown that a mixture of line spectral frequencies and partial correlation (PARCOR) coefficients can be...
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Automated storm tracking for terminal air traffic control
September 1, 1995
Journal Article
Published in:
Lincoln Laboratory Journal, Vol. 7, No. 2, Fall 1994, pp. 427-448.
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Summary
Good estimates of storm motion are essential to improved air traffic control operations during times of inclement weather. Automating such a service is a challenge, however, because meteorological phenomena exist as complex distributed systems that exhibit motion across a wide spectrum of scales. Even when viewed from a fixed perspective, these evolving dynamic systems can test the extent of our definition of motion, as well as any attempt at automated tracking of this motion. Image-based motion detection and processing appear to provide the best route toward robust performance of an automated tracking system.
Summary
Good estimates of storm motion are essential to improved air traffic control operations during times of inclement weather. Automating such a service is a challenge, however, because meteorological phenomena exist as complex distributed systems that exhibit motion across a wide spectrum of scales. Even when viewed from a fixed perspective...
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The Integrated Terminal Weather System terminal winds product
September 1, 1995
Journal Article
Published in:
Lincoln Laboratory Journal, Vol. 7, No. 2, Fall 1994, pp. 475-502.
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Summary
The wind in the airspace around an airport impacts both airport safety and operational efficiency. Knowledge of the wind helps controllers and automation systems merge streams of traffic; it is also important for the prediction of storm growth and decay, burn-off of fog and lifting of low ceilings, and wake vortex hazards. This knowledge is provided by the Integrated Terminal Weather System (ITWS) gridded wind product, or Terminal Winds. The Terminal Winds product combines data from a national numerical weather-prediction model, called the Rapid Update Cycle, with observations from ground stations, aircraft reports, and Doppler weather radars to provide estimates of the horizontal wind field in the terminal area. The Terminal Winds analysis differs from previous real-time winds-analysis systems in that it is dominated by Doppler weather-radar data. Terminal Winds uses an analysis called cascade of scales and a new winds-analysis technique based on least squares to take full advantage of the information contained in the diverse data set available in an ITWS. The weather radars provide sufficiently fine-scale winds information to support a 2-km horizontal-resolution analysis and a five-minute update rate. A prototype of the Terminal Winds analysis system was tested at Orlando International Airport in 1992, 1993, and 1995, and at Memphis International Airport in 1994. The field operations featured the first real-time winds analysis combining data from the Federal Aviation Administration TDWR radar and the National Weather Service NEXRAD radar. The evaluation plan is designed to capture both the overall system performance and the performance during convective weather, when the fine-scale analysis is expected to show its greatest benefit.
Summary
The wind in the airspace around an airport impacts both airport safety and operational efficiency. Knowledge of the wind helps controllers and automation systems merge streams of traffic; it is also important for the prediction of storm growth and decay, burn-off of fog and lifting of low ceilings, and wake...
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TCAS: maneuvering aircraft in the horizontal plane
September 1, 1995
Journal Article
Published in:
Lincoln Laboratory Journal, Vol. 7, No. 2, Fall 1994, pp. 295-312.
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Summary
The Traffic Alert and Collision Avoidance System (TCAS II) is now operating in all commercial airline aircraft to reduce the risk of midair collisions. TCAS II determines the relative positions of nearby aircraft, called intruders, by interrogating their transponders and receiving their replies. An intruder deemed a potential threat will trigger a resolution advisory (RA) that consists of an audible alert and directive that instructs the pilot to execute a vertical avoidance maneuver. Lincoln Laboratory has investigated the possibility of increasing the capability of TCAS II by incorporating the horizontal maneuvering of aircraft. Horizontal RAs can be computed if the intruder horizontal miss distances at closest approach are known. Horizontal miss distances can be estimated with range and bearing measurements of intruders. With this method, however, large errors in estimating the bearing rates will result in large errors in calculating the horizontal miss distances. An improved method of determining the horizontal miss distances may be to use the Mode S data link to obtain state data (position, velocity, and acceleration) from intruder aircraft.
Summary
The Traffic Alert and Collision Avoidance System (TCAS II) is now operating in all commercial airline aircraft to reduce the risk of midair collisions. TCAS II determines the relative positions of nearby aircraft, called intruders, by interrogating their transponders and receiving their replies. An intruder deemed a potential threat will...
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GPS antenna multipath rejection performance
August 7, 1995
Project Report
Published in:
MIT Lincoln Laboratory Report ATC-238
Summary
A GPS antenna multipath rejection performance evaluation was conducted at Lincoln Laboratory. Ground reference station antennas and aviation patches were tested for their ability to reject a muitipath signal. Different types of ground plane structures were used such as choke rings, ground planes, and mock sections of fuselage. Frequencies transmitted were L1 (1575 MHz), L2 (1227 MHz), and the median GLONASS frequency (1609 MHz ). Receive amplitude and phase were measured on each antenna. Subsequently, these data were converted to absoIute gain for a right-hand and Ieft- hand circularly polarized signal as a function of satellitte elevation angle. (Not Complete)
Summary
A GPS antenna multipath rejection performance evaluation was conducted at Lincoln Laboratory. Ground reference station antennas and aviation patches were tested for their ability to reject a muitipath signal. Different types of ground plane structures were used such as choke rings, ground planes, and mock sections of fuselage. Frequencies transmitted...
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