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51.
52.
<正>GF阿奇夏米尔作为欧洲最大的电加工和高速铣削机床厂商,其旗下的米克朗(MIKROH)系列高速高性能加工中心也正以不断拓宽的产品线在开拓铣削领域的市场份额。为 相似文献
53.
Tonissen S.M. Evans R.J. 《IEEE transactions on aerospace and electronic systems》1996,32(4):1440-1451
“Track-Before-Detect” (TBD) is a target tracking technique where no threshold is applied at each measurement frame. Instead, data are processed over a number of frames before decisions on target existence are made. The track is returned simultaneously with the detection. A simple algorithm is presented and demonstrated via simulations. A detailed analysis enables detection and tracking performance to be predicted for particular algorithm parameters. Good performance is observed at low signal-to-noise ratio (SNR), with rapid degradation as SNR is reduced further. For some cases the detection performance does not improve regardless of how many frames of data are processed. Tracking performance may also be poor even though detection performance is good 相似文献
54.
Sun-Mog Hong Evans R.J. Han-Seop Shin 《IEEE transactions on aerospace and electronic systems》2005,41(1):17-33
We address an optimization problem to obtain the combined sequence of waveform parameters (pulse amplitudes and lengths, and FM sweep rates) and detection thresholds for optimal range and range-rate tracking in clutter. The optimal combined sequence minimizes a tracking performance index under a set of parameter constraints. The performance index includes the probability of track loss and a function of estimation error covariances. The track loss probability and the error covariances are predicted using a hybrid conditional average algorithm. The effect of the false alarms and clutter interference is taken into account in the prediction. A measurement model in explicit form is also presented which is developed based on the resolution cell in the delay-Doppler plane for a single Gaussian pulse. Numerical experiments were performed to solve the optimization problem for several examples. 相似文献
55.
Musicki D. La Scala B.F. Evans R.J. 《IEEE transactions on aerospace and electronic systems》2007,43(4):1409-1425
A fully automatic tracking algorithm must be able to deal with an unknown number of targets, unknown target initiation and termination times, false measurements and possibly time-varying target trajectory behaviour. An efficient algorithm for tracking in this environment is presented here. This approach makes use of estimates of the probability of target existence, which is an integral part of the algorithm. This allows for the efficient generation and management of possible target hypotheses, yielding an algorithm with performance that matches what can be obtained by multiple hypothesis tracking-based approaches, but at a significantly lower computational cost. This paper considers only the single target case for clarity. The extension to multiple targets is easily incorporated into this framework. Simulation studies are given that show the effectiveness of this approach in the presence of heavy and nonuniform clutter when tracking a target in an environment of low probability of detection and in an environment where the target performs violent manoeuvres. 相似文献
56.
W.F.J. Evans R.S. OBrien 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1982,2(6):63-67
A scanning infrared radiometer used to measure nitric acid was flown on the STRATOPROBE Flight of November 8, 1978. Using the observed thermal emission from 6.5 to 7.4 microns during the balloon ascent, a water vapour profile has been derived using a band model of the water vapour lines in this spectral region. The resulting profile has a minimum of 3.3 ppmv at the tropopause and then rises to a value of 5 ppmv by 30 km. The profile is comparable to the profile from another water vapour instrument from the National Physical Laboratory which was flown on the LIP balloon payload on the same day. A coincident profile from the LIMS experiment on NIMBUS 7 was also obtained since the STRATOPROBE experiment was flown as a correlative measurement for the LIMS experiment. 相似文献
57.
The impact of dust grains on fast fly-by spacecraft: Momentum multiplication,measurements and theory
J.A.M. McDonnell T.J. Stevenson S.T. Evans M. Alexander D. Lyons W. Tanner P. Anz T. Hyde A.-L. Chen 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1984,4(9):297-301
Energy partitioning during the very high impact speed encountered in a cometary fly-by mission causes a target mass expulsion which leads to a momentum impulse on the target exceeding that of the incident momentum. Theoretical and computational studies are required to provide a basis for predictions of the response at Halley encounter, since experimental data from acceleration of microspheres extends currently only to some 10 kms?1. Such data obtained from the 2 MV Canterbury microparticle accelerator is presented: this demonstrates a target momentum enhancement E which can be approximated by a form E = 1+(V/Vo)β. Over the range 1 to 8 kms?1 the relationship is satisfied by Vo = 2 kms?1 and β = 2. Theoretical considerations of energy partitioning lead to constraints on the extrapolation of this functional dependence to very high velocities and the transition to β ≤ 1 is shown to apply. Results are examined and their significance to impact sensing and spacecraft deceleration discussed. An enhancement of momentum nearer to 12±3 at 69 kms?1 is anticipated for non-penetrating particles, from the ballistic pendulum data, but the ES data indicates a figure considerably higher. 相似文献
58.
J.W. Warwick J.H. Romig D.R. Evans 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1983,3(3):105-110
The Voyager observations of electrical discharges in Saturn's rings strongly support earlier speculations on the role played by electrostatics, magnetic fields, and lightning phenomena in the primitive solar system. They also suggest conditions then by direct analogy rather than by extrapolating backwards through time from conditions now. The observed discharges show a pronounced 10h periodicity, which suggests a source in Keplerian orbit at 1.80 ± 0.01 Saturn radii (1 RS = 60,330 km). In that region, the B ring is thicker than optical depth 1.8 for about 5,000 km. At 1.805 ± 0.001 Saturn radii, however, the ring is virtually transparent for a gap of width 200 m. We conclude that a small satellite orbits Saturn at that radius and clears the gap. The gap edges must prevent diffusive filling of the gap by fine material which is especially abundant at this position in the rings and would otherwise destroy the gap in minutes. The discharges represent the satellite's interaction with the outer edge of the gap. Spoke formation may involve the interaction of ring material in the vicinity of the gap. 相似文献
59.
Carlson B.D. Evans E.D. Wilson S.L. 《IEEE transactions on aerospace and electronic systems》1994,30(1):116-125
For pt.II see ibid., vol. 30, no 1, (Jan. 1994). This paper considers how well a Hough transform detector with binary integration improves the performance of a typical surveillance radar. For Hough transform detection, binary integration offers some advantages over noncoherent integration when multiple targets appear in range-time space or when the detector receives signals with a wide range of power. We derive expressions for PF and PD for a Hough transform binary integrator and apply the expressions to a typical surveillance radar. The results show that for the case considered, the binary Hough integrator improves the power budget of the radar by about 3 dB for a nonfluctuating target and 1 dB for a highly fluctuating target 相似文献
60.
The problems of satellite charges with reduced G/T stations for different pre-assigned and demand-assigned modes of operation are considered. A mixed pre-assigned demand-assigned operation is assumed as a model, in which large standard stations use the demand-assigned system for their overflow traffic. Determination of the optimum percentage of overflow for each link and of the global satellite revenue and occupancy, in terms of a general traffic matrix, is carried out and then used in the specific case of the Atlantic satellites to establish demand-assignment and pre-assignment charges as a function of G/T, based on a cost per unit bandwidth criterion. The effects of various demand-assignment systems on the economic balance is also considered. 相似文献