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SIDEWINDER MISSILE GPS RECEIVER TESTSMeyer, Steven J. 10 1900 (has links)
International Telemetering Conference Proceedings / October 25-28, 1999 / Riviera Hotel and Convention Center, Las Vegas, Nevada / The use of Global Positioning System (GPS) receivers as a source to provide Time Space
and Position Information (TSPI), and Miss Distance Indication (MDI) data in Test and
Evaluation (T&E) applications is being considered. Specifically, GPS receivers are being
evaluated to determine their usefulness as a sensor in a Sidewinder missile telemetry
system (AN/DKT-80). Initial testing has indicated that position information generated from
a GPS receiver can provide significantly better position data than a radar tracking system
when using Double Differential error correction techniques. This concept requires a GPS
reference station to be located in the general proximity of the Telemetry data-receiving
site. Software has been developed that will compare GPS data from the airborne telemetry
system to the GPS reference station and display a real-time TSPI solution. This software
will also provide MDI information from two different airborne sources that are equipped
with GPS receivers (missile and drone). To prove out this concept, a Commercial Off the
Shelf (COTS) Commercially/Available (C/A) code GPS receiver was integrated into the
AN/DKT-80 Sidewinder telemetry system (TM). A MQM-107 drone was instrumented
with the same GPS receiver, as was a ground based reference station. A simple TM was
developed for the drone that telemeters only the GPS data. The modified AN/DKT-80
system incorporated an Inertial Measurement Unit (IMU) into the design. Post processing
software was developed that will integrate the IMU information with the GPS data so
accurate position can be generated if the GPS data was momentarily lost. A missile firing
is scheduled for the spring of 1999 to prove this concept.
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TIME, SPACE, POSITION INFORMATION UNIT MESSAGE STRUCTURE OVERVIEWMeyer, Steven J. 10 1900 (has links)
International Telemetering Conference Proceedings / October 21, 2002 / Town & Country Hotel and Conference Center, San Diego, California / The Joint Advanced Missile Instrumentation (JAMI) program is developing a Time, Space, and Position Information (TSPI) unit for high dynamic missile platforms by employing the use of Global Position System (GPS) and inertial sensors. The GPS data is uncoupled from the inertial data. The output of the JAMI TSPI unit follows the packet telemetry protocol and is called the TSPI unit message structure (TUMS). The packet format allows the data stream to stand on its own, be integrated into a packet telemetry system or be an asynchronous data channel in a PCM data stream. On the ground, the JAMI data processor (JDP) Kalman filters the GPS and inertial data to provide a real time TSPI solution to the ranges for display. This paper gives an overview of the message format, the timing relationships between the GPS data and inertial data, and how TUMS is to be handled by the telemetry receiving site to hand it off to the JDP.
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INTEGRATING THE JOINT ADVANCED MISSILE INSTRUMENTATION (JAMI) TIME SPACE POSITION INFORMATION (TSPI) UNIT (JTU) INTO A TELEMETRY SYSTEMMeyer, Steven J. 10 1900 (has links)
ITC/USA 2005 Conference Proceedings / The Forty-First Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2005 / Riviera Hotel & Convention Center, Las Vegas, Nevada / The Joint Advance Missile Instrumentation (JAMI) program has developed a Time Space Position Information (TSPI) unit (JTU). The JTU employs a novel use of Global Positioning System (GPS) technology, and inertial measurement units (IMU) to provide a real time trajectory for high dynamic missile systems. The GPS system can function during high g maneuvers that an air-to-air missile might encounter. The IMU is decoupled from the GPS sensor. The IMU data is a secondary navigation source for the JTU and will provide platform attitude. The GPS data and IMU data are sent to the ground in telemetry packet called TSPI Unit Message Structure (TUMS). The TUMS packet is sent to a computer that hosts the JAMI Data Processing (JDP) software, which performs a Kalmam filter on the GPS and IMU data to provide a real time TSPI solution to the range displays. The packetized TUMS data is available in three different output formats: RS-232 serial data, 16-bit parallel and PCM. This paper focuses on how to integrate the JTU into a telemetry system, use it as a standalone system, and provides examples of possible uses.
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Using GPS for TSPI and Flight Termination Capabilities of a Missile Telemetry SectionKujiraoka, Scott R., Fielder, Russell G. 10 1900 (has links)
ITC/USA 2005 Conference Proceedings / The Forty-First Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2005 / Riviera Hotel & Convention Center, Las Vegas, Nevada / The Joint Advanced Missile Instrumentation (JAMI) Program involves the integration of Global Positioning System (GPS) tracking technology into the Test Ranges. GPS Technology will be used for Time, Space, and Position Information (TSPI) as well as Flight Termination purposes. JAMI is currently developing the JAMI TSPI Unit (JTU) and the Flight Termination Safe & Arm (FTS&A) devices. This paper will discuss the current efforts to integrate these JAMI components, off the shelf items (Flight Termination Receivers (FTR), Telemetry Transmitters, Encryptor and Thermal Batteries) and in-house developed devices (PCM Encoder, Tri-band Antenna with integrated Limiter, Filter, and Amplifier) into a five-inch diameter Missile Telemetry (TM) Section. The discussion of the transmission of the data and how the Test Ranges process it is beyond the scope of this paper and is covered in [1].
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Field Programmable Gate Array Application for Decoding IRIG-B Time CodeBrown, Jarrod P. 10 1900 (has links)
ITC/USA 2013 Conference Proceedings / The Forty-Ninth Annual International Telemetering Conference and Technical Exhibition / October 21-24, 2013 / Bally's Hotel & Convention Center, Las Vegas, NV / A field programmable gate array (FPGA) is used to decode Inter-Range Instrumentation Group (IRIG) time code for a PC-based Time-Space-Position Information (TSPI) acquisition. The FPGA architecture can latch time via an external event trigger or a programmable periodic internal event. By syncing time with an external IRIG Group Type B (IRIG-B) signal and using an 8 megahertz (MHz) internal clock, captured time has 125 nanosecond (ns) precision. A Range Instrumentation Control System (RICS) application utilizing the FPGA design to capture IRIG time is presented and test results show matching time accuracy when compared to commercial IRIG time capture hardware components.
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Factors Which Influence Key Entry Speed On Hard and Soft Keyboards: Experience, Eye Behaviors and Finger MovementsCelik, Seckin 01 January 2013 (has links) (PDF)
Soft keyboards have become ubiquitous, especially with the introduction of the iPad. This study aims to determine for experienced touch typists whether there are characteristics of soft QWERTY keyboards that can make them easier to use and why those characteristics provide an advantage. Two characteristics would appear to be of central importance. First, hard keyboards provide home row positioning information that is not as easily provided by soft keyboards. Second, hard keyboards also provide auditory and tactile feedback when a key is depressed, something not generally provided with soft keyboards.
In order to test the hypothesis that the absence of home row positioning and key strike feedback information can reduce expert touch typists’ speeds on soft keyboards, expert touch typists were run in two experiments. In Experiment 1, soft and hard keyboards in landscape and portrait mode were evaluated. The hard keyboards had the standard home row positioning and key strike feedback whereas the soft keyboards had neither. If these are important elements in typing speed, then experienced hard keyboard typists should type less quickly when using soft keyboards than when using hard keyboards. Moreover, if reducing the footprint of the keyboard, from landscape to portrait, requires more eye movements, then typists using both hard and soft keyboards should be slower when using the portrait size keyboard than when using the landscape size keyboard. Perhaps not surprisingly, experienced hard keyboard touch typists do less well when entering information on soft keyboards without home row positioning information or auditory feedback. Moreover, both groups appear to type more slowly in keyboards laid out in a portrait format than they do in keyboards laid out in a landscape format.
In summary, the results from Experiment 1 suggest that both home row positioning information and auditory key strike feedback should speed performance. In Experiment 2, an attempt was made to determine just how much of a gain can be made in the typing speed of more experienced soft keyboard users if home row positioning information (tactile feedback), auditory feedback, or both are added. Participants were run in four conditions: auditory key strike feedback (with and without) was crossed with tactile home row positioning information (with and without). Participants included expert level hard keypad QWERTY touch typists who have had at least five hours’ typing experience with an iPad. Participants were given four passages to type, all of equal length and all balanced for letter frequency. Participants typed one passage in each of the four conditions. The passage sequence was counterbalanced across participants. Typing speeds for each of the passages was measured and averaged across participants within conditions. A repeated measures analysis of variance was used to determine whether there was a main effect of position or feedback.
In order to determine why it is that home row positioning and key strike feedback alters performance, eye behaviors, movement times and task completion times are calculated. If home row position information is important, soft keyboards without this information may have a larger number of glances that a typist directs at the keyboard. These glances will help the typist determine either whether a finger is positioned over the correct home key (the launch key) or whether the location of the key to be typed next (the target key) is in the expected position. If key strike feedback is important, soft keyboards without this information should have longer movement times where the typists do not need to glance at the keyboard. This follows since the typist will process less quickly the fact that a finger has landed on a key.
Key press and key release times will be included each time a character, number or spacebar is depressed or releases. The finger movement time between any pair of keys i and j will be derived from the key press and key release times. This time will be measured from the moment the finger leaves the launch key i until the moment that the finger arrives at the target key j. Task completion times were defined as the difference between the first key press in a passage and the last key release. Finger movement times, inter-keystroke intervals and task completion times were recorded using a program developed in JAVA 2SE. Eye movements are recorded with aid of an ASL Mobile EYE tracker.
Analyses of the finger movement times and task completions times in Experiment 2 indicated that participants were fastest when both position information and auditory feedback were included. When just finger movement times are considered, there was a significant effect of auditory feedback but not of positioning information. This was what was expected given that the speed of finger movement times is arguably largely a function of how quickly a typist perceives that a movement has been completed, something that auditory feedback, but not positioning information provides. When just the task completion times were analyzed, position information had a significant effect. The effect of auditory feedback was only marginally significant. It was expected that both factors would be significant. Perhaps the power was too small. Finally, when the eye movements were analyzed, the total scanning time was shortest when both position information and auditory feedback were available. The effects of both were statistically significant.
In summary, on the basis of the results from Experiment 1 it appeared likely that auditory feedback and positioning information accounted in part for the faster typing times of touch typists on hard keyboards as opposed to soft keyboards. In Experiment 2, this hypothesis was evaluated. Finger movement and task completion times were fastest when both auditory feedback and positioning information were present. The effect of auditory feedback appeared to impact only the finger movement times. The effect of both auditory feedback and positioning information appeared to impact the task completion times. However, the effect of auditory feedback on task completion times was only marginal. Finally, it was clear that much of the reduction in task completion times occurred because the time that the touch typists spent scanning the keyboard was smaller when both auditory feedback and positioning information was available.
It is recommended in the future that soft keyboards have both sets of feedback available, auditory (through simulated key clicks) and tactile (through home row positioning information). The gains in typing speed with these additions were models (about 10%), considered over the entire population of users the impact could be considerable.
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USING COOPERATIVE RESEARCH AND DEVELOPMENT AGREEMENTS (CRADA) TO REDUCE THE TRANSITION TO PRODUCTION RISK OF A MISSILE TELEMETRY SECTIONKujiraoka, Scott R., Fielder, Russell G. 10 1900 (has links)
ITC/USA 2007 Conference Proceedings / The Forty-Third Annual International Telemetering Conference and Technical Exhibition / October 22-25, 2007 / Riviera Hotel & Convention Center, Las Vegas, Nevada / The Joint Advanced Missile Instrumentation (JAMI) Program’s main thrust has
been the integration of Global Positioning System (GPS) tracking technology into the
Department of Defense (DoD) Missile Test Ranges. This technology could be used for
Time, Space, Position, and Information (TSPI), Flight Termination (FTS), or End Game
Scoring purposes. However the Program’s main goal is to develop Proof-of-Concept
components only. Transitioning Missile technology developed by the Government to
Private Industry, so that it can be economically mass produced, has been quite a
challenge. Traditionally, private industry has had to bid on proposals without much
detailed information on how these components have been designed and fabricated.
These unknown risks, Non-Recurring Engineering (NRE) and Missile Flight Qualification
costs, routinely have significantly increased the price of these procurement contracts.
In order so that the Fleet can economically utilize these components in the field,
Cooperative Research and Development Agreements (CRADA) between the
Government and Private Industry have been used to successfully transition Government
developed technology to mass production. They can eliminate the NRE and flight
qualification costs to provide for an economical and low risk method of providing the
Fleet with the latest advances in GPS Tracking Technology. This paper will discuss
how this is currently being accomplished in the development of a conformal wraparound
instrumentation antenna for a five-inch diameter Missile Telemetry (TM) Section.
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TRANSPORTABLE RANGE AUGMENTATION AND CONTROL SYSTEMS FOR MULTIPLE SHOT ENGAGEMENTSGlenn, Tom, Chavez, Tomas, Toole, Michael T., Markwardt, Jack 11 1900 (has links)
International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, Las Vegas, Nevada / The Ballistic Missile Defense Organization (BMDO) is developing new Theater
Missile Defense (TMD) weapon systems to defend against the rapidly expanding
ballistic missile threat. The tactical ballistic missile threats include systems with range
capabilities greater than 1000 kilometers. The development and testing of systems
such as the Patriot Advanced Capability 3 (PAC-3), the Theater High Altitude Area
Defense (THAAD), Navy Area Defense, and the System Integration Tests (SIT) to
address the interoperability of this family of systems, will require the development of
the Transportable Range Augmentation and Control System for Multiple Shot
Engagements (TRACS - MSE). Congress has mandated that these systems be tested in
multiple simultaneous engagements. These systems will be tested at several ranges to
meet all the developmental and operational testers' needs. Potential range locations
include White Sands Missile Range (WSMR), Kwajalein Missile Range (KMR), the
Pacific Missile Range Facility (PMRF) and the Gulf Range at Eglin Air Force Base.
Due to the long distances separating the target launch site and the interceptor site, the
TRACS - MSE will be required at multiple sites for each range used. To be cost
effective, transportable systems should be developed to augment existing capabilities.
Advances in Global Positioning System (GPS) technology and high data rate receivers
make telemetry based solutions attractive. This article will address the requirements
for range safety, for Time, Space, Position Information (TSPI) collection and
processing requirements to support a TRACS - MSE capability.
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TELEMETRY CHALLENGES FOR BALLISTIC MISSILE TESTING IN THE CENTRAL PACIFICMarkwardt, Jack, LaPoint, Steve 10 1900 (has links)
International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and Convention Center, San Diego, California / The Ballistic Missile Defense Organization (BMDO) is developing new Theater Missile
Defense (TMD) and National Missile Defense (NMD) weapon systems to defend against
the expanding ballistic missile threat. In the arms control arena, theater ballistic missile
threats have been defined to include systems with reentry velocities up to five kilometers
per second and strategic ballistic missile threats have reentry velocities that exceed five
kilometers per second. The development and testing of TMD systems such as the Army
Theater High Altitude Area Defense (THAAD) and the Navy Area Theater Ballistic
Missile Defense (TBMD) Lower Tier, and NMD systems such as the Army
Exoatmospheric Kill Vehicle and the Army Ground-Based Radar, pose exceptional
challenges that stem from extreme acquisition range and high telemetry data transfer rates.
Potential Central Pacific range locations include U.S. Army Kwajalien Atoll/Kwajalein
Missile Range (USAKA/KMR) and the Pacific Missile Range Facility (PMRF) with target
launches from Vandenberg Air Force Base, Wake Island, Aur Atoll, Johnston Island, and,
possibly, an airborne platform. Safety considerations for remote target launches dictate
utilization of high-data-rate, on-board instrumentation; technical performance measurement
dictates transmission of focal plane array data; and operational requirements dictate
intercepts at exoatmospheric altitudes and long slant ranges. The high gain, high data rate,
telemetry acquisition requirements, coupled with loss of the upper S-band spectrum, may
require innovative approaches to minimize electronic noise, maximize telemetry system
gain, and fully utilize the limited S-band telemetry spectrum. The paper will address the
emerging requirements and will explore the telemetry design trade space.
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Space Tracking Systems/ Options StudyGrelck, John, Ehrsam, Eldon, Means, James A. 10 1900 (has links)
International Telemetering Conference Proceedings / October 17-20, 1994 / Town & Country Hotel and Conference Center, San Diego, California / This paper presents the findings of the Space Tracking Systems/Options Study (STS/OS) and indicates its impact on the telemetering community. The STS/OS was commissioned by Air Force Test & Evaluation (AF/TE) to develop a long range plan (vision and roadmap) for the AF Test & Evaluation (T&E) community to ensure affordable capabilities (telemetry, tracking and commanding) for the future (2003-2008). The study was conducted by the Air Force Materiel Command (AFMC), Space & Missile Systems Center (SMC), Detachment 9, at Vandenberg AFB (VAFB), with support from the primary AFMC T&E centers, the Air Force Operational Test & Evaluation Command (AFOTEC), and the Air Force Space Command (AFSPC). Both "open air" aeronautical and astronautical test needs were considered. The study solicited requirements for existing and future programs, extrapolated existing and planned test capabilities out into the future, then compared the two to identify future shortfalls in capabilities and specific actions that are necessary to insure that the future program needs can be met. Three critical types of testing were identified that cannot be satisfied with existing or planned instrumentation. These are: large area testing (LAT), over the horizon testing (OTH), and space weapons testing (SWT). A major deficiency was also uncovered in end game scoring for air and space intercepts, where inadequate capability exists to perform the required vector miss-distance measurement. This paper is important to the telemetering community because it identifies the Global Positioning System (GPS) as the primary time space position information (TSPI) system for all future open air testing. GPS provides a passive capability that permits each vehicle to determine its own precise TSPI. Means must be provided, however, for the vehicle to relay its position to the appropriate range control center. The paper shows that the problems with down linking telemetry, aircraft buss data, digital audio, digital video, and TSPI collectively represent the need for a very capable datalink. Likewise, the need to uplink commands, synthetic targets, synthetic backgrounds, and target control information also represents the need for a very capable datalink. With its extensive expertise in RF linkages, the telemetering community is ideally suited to address this need for a robust datalink for the future of T&E.
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