Modeling Space in the Air Force Command Exercise System (ACES)

In response to the increased influence of space forces on today\u27s battlefield, several theater level models were analyzed for the presentation of space forces. These models were the Extended Air Defense Simulation (EADSIM), the Joint Theater Level Simulation (JTLS), the Integrated Theater Engagement Model (ITEM), the Tactical Warfare Model (TACWAR), Thunder, Janus, and the Aggregate Level Simulation Protocol (ALSP). While ALSP is not a model but a simulation protocol connecting various models, it was studied because it appears to be the future of modeling. The consensus of the analysis was that space forces are virtually ignored by most of the models and when space was considered, the dynamic nature of the systems involved were not captured. The Air Force Cornmand Exercise System (ACES) was chosen to determine how the effects of space forces can be implemented into theater level models. ACES is a discrete event combat simulation designed to support intermediate and senior service schools in teaching Air Force doctrine within the context of a theater warfare exercise. Its primary focus is to allow specific educational goals to be taught. This research focused on both the present modeling of space forces within widely used theater level models and a methodology to incorporate space forces into models that lack the influence of space. The Gulf War exposed how important functions performed from space can be to the success of a combat forces. Because of the practicality of space\u27s influence, a picture of today\u27s battlefield that does not include space forces is incomplete

NA

Distinguished Alumni Award Program author. The Honorable Thomas White, Secretary of the Army. NPS Hall of Fame Author (Presented September 27, 2001)Tactical ECM planning has historically considered only horizontal positioning of self-protection and standoff jamming systems. Failure to consider vertical positioning of the jammer, and how the environment affects that positioning, can lead to substantially reduced jamming effectiveness. The effects of radar and jamming system antenna patterns and environmental considerations are discussed. The Integrated Refractive Effects Prediction System (IREPS) incorporates these effects, but not in a form that is convenient for ECM planning. However, as it is now configured, IREPS can be a useful tool. A step-by-step approach for using IREPS and the jamming equations to assist the ECM planner is given. Sample calculations for self-protection and standoff jamming under actual environmental conditions are provided.http://archive.org/details/positioningofjam00whitNAN

Tactical Electronics Simulation Test System: Final Report CDRL A004

Report addresses the preliminary findings of the Tactical Electronics Simulation Test System (TESTS) Phase I effort: Requirements Analysis and Feasibility Assessment, involving requirements for an advanced identification friend or foe (IFF) simulation environment, existing applicable and available facilities and resources for subsequent project phases, technical issues and concerns to minimize risk, and technical approach and conceptual design for an advanced IFF system and environment simulation leading to TESTS

Adaptive estimation and equalisation of the high frequency communications channel

SIGLEAvailable from British Library Document Supply Centre- DSC:D94945 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Time and Frequency Transfer in a Coherent Multistatic Radar using a White Rabbit Network

Networks of coherent multistatic radars require accurate and stable time and frequency transfer (TFT) for range and Doppler estimation. TFT techniques based on global navigation satellite systems (GNSS), have been favoured for several reasons, such as enabling node mobility through wireless operation, geospatial referencing, and atomic clock level time and frequency stability. However, such systems are liable to GNSS-denial, where the GNSS carrier is temporarily or permanently removed. A denial-resilient system should consider alternative TFT techniques, such as the White Rabbit (WR) project. WR is an Ethernet based protocol, that is able to synchronise thousands of nodes on a fibre-optic based network with sub-nanosecond accuracy and picoseconds of jitter. This thesis evaluates WR as the TFT network for a coherent multistatic pulse-Doppler radar – NeXtRAD. To test the hypothesis that WR is suitable for TFT in a coherent multistatic radar, the time and frequency performance of a WR network was evaluated under laboratory conditions, comparing the results against a network of multi-channel GPS-disciplined oscillators (GPSDO). A WR-disciplined oscillator (WRDO) is introduced, which has the short-term stability of an ovenised crystal (OCXO), and long-term stability of the WR network. The radar references were measured using a dual mixer time difference technique (DMTD), which allows the phase to be measured with femtosecond level resolution. All references achieved the stringent time and frequency requirements for short-term coherent bistatic operation, however the GPSDOs and WRDOs had the best short-term frequency stability. The GPSDOs had the highest amount of long-term phase drift, with a peak-peak time error of 9.6 ns, whilst the WRDOs were typically stable to within 0.4 ns, but encountered transient phase excursions to 1.5 ns. The TFT networks were then used on the NeXtRAD radar, where a lighthouse, Roman Rock, was used as a static target to evaluate the time and frequency performance of the references on a real system. The results conform well to the laboratory measurements, and therefore, WR can be used for TFT in coherent radar

Abstracts on Radio Direction Finding (1899 - 1995)

The files on this record represent the various databases that originally composed the CD-ROM issue of "Abstracts on Radio Direction Finding" database, which is now part of the Dudley Knox Library's Abstracts and Selected Full Text Documents on Radio Direction Finding (1899 - 1995) Collection. (See Calhoun record https://calhoun.nps.edu/handle/10945/57364 for further information on this collection and the bibliography). Due to issues of technological obsolescence preventing current and future audiences from accessing the bibliography, DKL exported and converted into the three files on this record the various databases contained in the CD-ROM. The contents of these files are: 1) RDFA_CompleteBibliography_xls.zip [RDFA_CompleteBibliography.xls: Metadata for the complete bibliography, in Excel 97-2003 Workbook format; RDFA_Glossary.xls: Glossary of terms, in Excel 97-2003 Workbookformat; RDFA_Biographies.xls: Biographies of leading figures, in Excel 97-2003 Workbook format]; 2) RDFA_CompleteBibliography_csv.zip [RDFA_CompleteBibliography.TXT: Metadata for the complete bibliography, in CSV format; RDFA_Glossary.TXT: Glossary of terms, in CSV format; RDFA_Biographies.TXT: Biographies of leading figures, in CSV format]; 3) RDFA_CompleteBibliography.pdf: A human readable display of the bibliographic data, as a means of double-checking any possible deviations due to conversion

An investigation of the microwave upset of avionic circuitry

Circuit technology of the 1970-90 era appears fairly resilient to microwave radio frequency interference, with few reported occurrences of interference. However, a proposition has been developed which substantiates fears that new technologies, with their extremely high packing densities, small device p-n junctions and very high clock rates, will be very susceptible to interference throughout the microwave band It has been postulated that the mechanism for this upset is demodulation and that it will come about by either the predicted changes in the microwave RF environment by the year 2000, or by a suitable choice of phasing and frequency at high power. The postulation is studied by developing an overall ingress equation, relating incident power density at the aircraft to the load voltage at an avionic circuit component. The equation's terms are investigated to quantif' their contribution to the likelihood of interference. The operational RF environment for aircraft is studied and predictions of the current and maximum future environments are made. A practical investigation of 2-18 GH.z airframe shielding is described, with comparison of the results with those from a number of other aircraft and helicopter types. A study of ingress into avionic boxes is presented and is followed by the results of an investigation of energy coupling via the cables and connectors, including the development and practical examination of a coupling model based on transmission line theory. A study is then presented of circuit technology developments, electronic component interference and damage mechanisms, and evidence of upset of electronic equipment is given. Investigations show that there is more 1-18 GHz upset of electronic equipment than originally thought and data suggest that thermal damage of active devices may dominate over-voltage stressing of p-n junctions. Aircraft investigations have shown that incident microwave radiation is attenuated approximately 20 dB by the airframe, in a complex fashion which does not lend itself to being modelled easily. Under some conditions this value of airframe attenuation is seen to approach zero, removing any shielding of avionics by the airframe for these cases. A predictor for airframe shielding independent of air vehicle type has been developed, based on cumulative density ftrnctions of all data from each of the aircraft types examined. The cable coupling model gives good agreement with measured data except for the dependency of load voltage on cable length and illuminating antenna position along the cable, for which an empirical equation has been developed. Computer power limitations and significant variations of most of the parameters in the overall ingress equation suggest that modelling of the complex innards of aircraft and avionics at these frequencies will remain impractical for the foreseeable future and that probabilistic models are the only achievable goal. It is concluded that all avionic circuit technologies may well be upset as postulated above or by speculative High Power Microwave weapons, but that careful use of existing aircraft and equipment design methodologies can offer adequate protection. An improved protection regime is proposed for future aircraft and a number of fUture research areas are identified to enable better understanding of the microwave hazard to aircraft. The three areas which will add most to this understanding are modelling of the precise microwave environment to be encountered, further airframe shielding measurements and analyses, from all incidence angles and on different aircraft types, and the construction and cumulative probability fUnction analyses of electronic component and equipment upset databases

1995 BRAC Commission

DoD Depots - Presentation; Itinerary; Manpower authorizations; Output and operating expenses; Environmental Impact. Box 270, XS-006

1995 BRAC Commission

Executive Correspondence Tracking System #13 - April 1995 (950420-10 TO 95425-17). Box 52, C-108