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901.
Train control has three major functions: (1) protection; (2) operation; and (3) supervision. These functions of train control have been (and still are) implemented both manually and automatically at various railways. The first of these functions, train protection, prevents trains from traveling onto sections of track where they could collide with another train or derail due to switch positions. It also prevents trains from exceeding the safe operating speed, as determined by the vehicle type and track geometry (curves and gradients). The second function, train operation, involves the guidance of a single train in motion and at rest, when it is operating within the train protection function. Finally, train supervision involves guiding and recording the progress of multiple trains in an effort to provide economies to, or assign priorities throughout, the overall railway 相似文献
902.
W G Sannita M Acquaviva S L Ball F Belli S Bisti V Bidoli S Carozzo M Casolino F Cucinotta M P De Pascale L Di Fino S Di Marco R Maccarone C Martello J Miller L Narici N S Peachey P Picozza A Rinaldi D Ruggieri M Saturno D Schardt M Vazquez 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,33(8):1347-1351
ALTEA-MICE will supplement the ALTEA project on astronauts and provide information on the functional visual impairment possibly induced by heavy ions during prolonged operations in microgravity. Goals of ALTEA-MICE are: (1) to investigate the effects of heavy ions on the visual system of normal and mutant mice with retinal defects; (2) to define reliable experimental conditions for space research; and (3) to develop animal models to study the physiological consequences of space travels on humans. Remotely controlled mouse setup, applied electrophysiological recording methods, remote particle monitoring, and experimental procedures were developed and tested. The project has proved feasible under laboratory-controlled conditions comparable in important aspects to those of astronauts' exposure to particle in space. Experiments are performed at the Brookhaven National Laboratories [BNL] (Upton, NY, USA) and the Gesellschaft für Schwerionenforschung mbH [GSI]/Biophysik (Darmstadt, FRG) to identify possible electrophysiological changes and/or activation of protective mechanisms in response to pulsed radiation. Offline data analyses are in progress and observations are still anecdotal. Electrophysiological changes after pulsed radiation are within the limits of spontaneous variability under anesthesia, with only indirect evidence of possible retinal/cortical responses. Immunostaining showed changes (e.g. increased expression of FGF2 protein in the outer nuclear layer) suggesting a retinal stress reaction to high-energy particles of potential relevance in space. 相似文献
903.
J L Huntington D M Stratton T W Scattergood 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1995,15(3):135-138
The Gas-Grain Simulation Facility (GGSF) is a multidisciplinary experiment laboratory being developed by NASA at Ames Research Center for delivery to Space Station Freedom in 1998. This facility will employ the low-gravity environment of the Space Station to enable aerosol experiments of much longer duration than is possible in any ground-based laboratory. Studies of fractal aggregates that are impossible to sustain on Earth will also be enabled. Three research areas within exobiology that will benefit from the GGSF are described here. An analysis of the needs of this research and of other suggested experiments has produced a list of science requirements which the facility design must accommodate. A GGSF design concept developed in the first stage of flight hardware development to meet these requirements is also described. 相似文献
904.
The two-stage Kalman estimator has been studied for state estimation in the presence of random bias and applied to the tracking of maneuvering targets by treating the target acceleration as a bias vector. Since the target acceleration is considered a bias, the first stage contains a constant velocity motion model and estimates the target position and velocity, while the second stage estimates the target acceleration when a maneuver is detected, the acceleration estimate is used to correct the estimates of the first stage. The interacting acceleration compensation (IAC) algorithm is proposed to overcome the requirement of explicit maneuver detection of the two-stage estimator. The IAC algorithm is viewed as a two-stage estimator having two acceleration models: the zero acceleration of the constant velocity model and a constant acceleration model. The interacting multiple model (IMM) algorithm is used to compute the acceleration estimates that compensate the estimate of the constant velocity filter. Simulation results indicate the tracking performance of the IAC algorithm approaches that of a comparative IMM algorithm while requiring approximately 50% of the computations 相似文献
905.
Masserant B.J. Beans E.W. Stuart T.A. 《IEEE transactions on aerospace and electronic systems》1995,31(1):280-287
Earlier references have described a new soft switched ZVS/ZCS (zero voltage switching, zero current switching) converter for IGBTs that allows operation above 20 kHz. Although frequencies above 20 kHz are now possible for IGBT converters, the optimum frequency for minimum volume may be below 20 kHz because of heat sink requirements. A comparative study considers the reactive component versus heat sink volume tradeoff for two 6 kW converters, one using ZVS/ZCS and the other using a more conventional circuit with hard switching 相似文献
906.
Flight path estimation using frequency measurements from a wideaperture acoustic array 总被引:1,自引:0,他引:1
A narrowband technique based on the acoustical Doppler effect is proposed for estimating the trajectory of a turbo-prop aircraft in level flight with constant velocity as it transits over a ground-based passive acoustic sensor array. The basic principle is to measure the temporal variation of the instantaneous frequency (IF) of the acoustic signal received by each sensor and then to minimize the sum of the squared deviations of the IF estimates from their predicted values over a sufficiently long period of time for all sensors. The technique provides estimates of the propeller blade rate and the five source motion parameters that describe the aircraft trajectory. The six dimensional minimization problem is reduced to a five dimensional maximization problem, which is solved numerically using the quasi-Newton method. A simple method is described that provides the initial parameter estimates required for the numerical maximization. The effectiveness of the motion parameter estimation technique is verified using real acoustic data recorded from a wide aperture microphone array during various transits of a turbo-prop aircraft 相似文献
907.
R. W. Schunk T. -Z. Ma 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1995,15(12):107-110
The field-aligned expansion of plasma clouds in the ionosphere was studied with different mathematical models and for a wide range of conditions. In all cases, the expanding plasma cloud acted as an electrostatic snowplow, creating an O+ hole in the ionosphere coincident with the cloud and O+ bumps on the two sides of the cloud that are aligned with the geomagnetic field. 相似文献
908.
It is argued that human factors professionals in large R&D organizations should have a centralized human factors group (or department) with a manager sensitive to human factors organizational issues. This arrangement permits these professionals to maximize their contributions to the design, development, and testing of a product or service. Managers of human factors groups and departments can help educated project managers about the value of human factors. Human factors groups, departments, and managers provide benefits to the company by resolving project conflicts concerning user-oriented designs. They help foster a sense of a behavioral sciences community within the R&D organization and aid in recruiting job candidates. They are good for the product or service, the company, and the human factors profession 相似文献
909.
McCormick W.S. Miller D.E. Tsui J.B.Y. 《IEEE transactions on aerospace and electronic systems》1995,31(1):2-8
An algorithm is proposed to resolve a fundamental 2π ambiguity problem occurring in multiple frequency spectral estimation. Given M frequencies fm, and I separate frequency estimators with unambiguous bandwidths Fi, the ambiguity problem can be stated as solving for the fm, given the estimator outputs, αmi, (1⩽m⩽M;1⩽i⩽I) where fm=αmi+KmiFi and Kmi is some integer. The proposed algorithm exhaustively resolves all possible αmi groupings into single frequency values using a noise insensitive technique that exchanges system bandwidth for noise protection. The correct multiple frequencies are then defined as the single frequencies that repeat a specified number of times. A complete analysis is included 相似文献
910.
Thompson M.W. Ho-Shin Chang 《IEEE transactions on aerospace and electronic systems》1994,30(2):452-461
The discrete-time detection of a time-varying, additive signal in independent Laplace noise is considered. Previous efforts in this area have been restricted to the constant signal, and identically distributed noise case. Theoretical (closed form) expressions for the false alarm and detection probabilities are developed for both the Neyman-Pearson optimal detector and the classical matched filter detector. Comparisons between the two detectors are made which illustrate the effects of signal-to-noise power ratio and sample size for certain false alarm and detection probability constraints. In view of the fact that the optimal Laplace detector is not UMP, we also investigate the effect of signal amplitude mismatch 相似文献