Spelling suggestions: "subject:"codetermination"" "subject:"codétermination""
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ENHANCED FLIGHT TERMINATION SYSTEM PROGRAM - PART TWOMcAndrews, Thomas J., III 10 1900 (has links)
International Telemetering Conference Proceedings / October 21, 2002 / Town & Country Hotel and Conference Center, San Diego, California / The Air Force Flight Test Center in association with the Range Commanders Council (RCC) Range Safety Group is conducting a program that will explore the next generation of ground-based flight termination technology, known as the Enhanced Flight Termination System (EFTS) program. The first part of the program was successfully concluded in May 2002. The Government is leading this program with support from contractors, academia, and other RCC groups including the Telemetry Group, Frequency Management Group, and Telecommunications and Timing Group. Additionally, the National Security Agency is providing key support along with vendors who design, build and test range safety systems. This paper will discuss details of the design validation and development phases (part two) of the EFTS program. Redesign of flight termination receivers and ground system modification plans will be discussed as well as flight and ground hardware testing objectives.
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A STATUS REPORT OF THE JOINT ADVANCED MISSILE INSTRUMENTATION PROJECT JAMI SYSTEM INTEGRATIONPowell, Dave 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 / Joint Advanced Missile Instrumentation (JAMI), a Central Test and Evaluation Investment Program (CTEIP) initiative, is developing advanced telemetry system components that can be used in an integrated instrumentation package for tri-service small missile test and training applications. JAMI demonstrated significant improvement in the performance of low-cost Global Positioning System (GPS) based Time-Space-Position Information (TSPI) tracking hardware that can be used for world-wide test and training. Acquisition times of less than 3 seconds from a cold start and tracking dynamics to over 60Gs were demonstrated. The final production designs and flight testing results are discussed along with comparisons to the initial project requirements. A discussion of integration initiatives and implementation issues are included.
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Diffusive shock acceleration in the solar systemSavopulos, Mihail January 1995 (has links)
No description available.
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Free radical polymerisation studies of 4-substituted styrenesLudlow, Andrew John January 1995 (has links)
No description available.
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Behavior of the James Lobe, South Dakota during Termination IHeath, Stephanie L. 18 October 2019 (has links)
No description available.
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PREMATURE TERMINATION: THE PATIENT'S PERSPECTIVEReynolds, David Jerome 11 October 2001 (has links)
No description available.
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Disposable Workers: Race, Gender, and Firing DiscriminationByron, Reginald Anthony 11 September 2009 (has links)
No description available.
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Re-thinking termination guarantee of eBPFSahu, Raj 10 June 2024 (has links)
In the rapidly evolving landscape of BPF as kernel extensions, where the industry is deploying an increasing count of simultaneously running BPF programs, the need for accounting BPF- induced overhead on latency-sensitive kernel functions is becoming critical. We also find that eBPF's termination guarantee is insufficient to protect systems from BPF programs running extraordinarily long due to compute-heavy operations and runtime factors such as contention. Operators lack a crucial mechanism to identify and avoid installing long-running BPF programs while also requiring a mechanism to abort such BPF programs when found to be adding high latency overhead on performance-critical kernel functions. In this work, we propose a runtime estimator and a dynamic termination mechanism to solve these two issues, respectively. We use a hybrid of static and dynamic analysis to provide a runtime range that we demonstrate to encompass the actual runtime of the BPF program. For safe BPF termination, we propose a short-circuiting approach to skip all costly operations and quickly reach completion. We evaluate the proposed solutions to find the obtained performance estimate as too broad, but when paired with the dynamic termination, can be used by a BPF Orchestrator to impose policies on the overhead due to BPF programs in a call path. The proposed dynamic termination solution has zero overhead on BPF programs for no-termination cases while having a verification overhead proportional to the number of helper calls in a BPF program. In the future, we aim to make BPF execution atomic to guarantee that kernel objects modified within a BPF program are always left in a consistent state in the event of program termination. / Master of Science / The Linux kernel OS has a relatively recent feature called eBPF which allows adding new code into a running system without needing a system reboot. Due to the flexibility offered by eBPF, the technology is attracting widespread adoption for diverse use cases such as system health monitoring, security, accelerating programs, etc. In this work, we identify that eBPF programs have a non-negligible performance impact on a system which, in the extreme case, can cause Denial-of-Service attacks on the host machine despite going through all security checks enforced by eBPF. We propose a two-part solution: the eBPF runtime estimator and the Fast-Path termination mechanism. The runtime estimator aims to prevent the instal- lation of eBPF programs that can cause a large performance impact, while the Fast-Path termination will act as a safety net for cases when the installed program unexpectedly runs longer. The overall solution will enable better management of eBPF programs concerning their performance impact and enforce strict bounds on the added latency. Potential future work includes factoring in the impacts other than performance in our solution such as inter- BPF interaction and designing easy-to-use knobs which an operator can easily tune to relax or constrain the side-effects of the eBPF programs installed in the system.
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Active, Passive and Active/Passive Control Techniques For Reduction of Vibrational Power Flow in Fluid Filled PipesKartha, Satish Chandrashekhar 24 February 2000 (has links)
The coupled nature of vibrational energy flow in fluid filled piping systems makes its control and subsequent reduction a difficult problem. This work experimentally explores the potential of different active, passive and active/passive control methodologies for control of vibrational power flow in fluid filled pipes. Circumferential modal decomposition and measurements of vibrational power carried by individual wave types were carried out experimentally. The importance of dominant structural bending waves and the need to eliminate them in order to obtain meaningful experimental results has been demonstrated. The effectiveness of the rubber isolator in reducing structural waves has been demonstrated. Improved performance of the quarter wavelength tube and Helmholtz resonator was obtained on implementation of the rubber isolator on the experimental rig. Active control experiments using the side-branch actuator and 1/3 piezoelectric composite yielded significant dB reductions revealing their potential for practical applications. A combined active/passive approach was also implemented as part of this work. This approach yielded promising results, which proved that combining advantages of both active and passive approaches was a feasible alternative. / Master of Science
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ENHANCED FLIGHT TERMINATION SYSTEM FLIGHT DEMONSTRATION AND RESULTSTow, David, Arce, Dennis 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 / This paper discusses the methodology, requirements, tests, and implementation plan for the live
demonstration of the Enhanced Flight Termination System (EFTS) using a missile program at
two locations in Florida: Eglin Air Force Base (AFB) and Tyndall AFB. The demonstration
included the integration of EFTS Flight Termination Receivers (FTRs) onto the missile and the
integration of EFTS-program-developed transmitter assets with the mission control system at
Eglin and Tyndall AFBs. The initial test stages included ground testing and captive-carry flights,
followed by a launch in which EFTS was designated as the primary flight termination system for
the launch.
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