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241.
Fisher H.L. Musser K.L. Shuster M.D. 《IEEE transactions on aerospace and electronic systems》1993,29(1):22-26
Attitude estimation algorithms for the Thrusted Vector Mission which determine attitude based on Sun sensor and very coarse albedo sensor measurements are presented. On the basis of these measurements, it has been demonstrated by comparison with more accurate gyro-based attitude that it is possible to estimate three-axis attitude with an average error per axis of 11 deg. Most of this error is about the Sun direction. Both deterministic quick-look and optimal estimates are examined 相似文献
242.
Zeitz F.H. III Maybeck P.S. 《IEEE transactions on aerospace and electronic systems》1993,29(4):1123-1136
The discrete-time Kalman filter is an optimal estimator for the states of a linear, stochastic system. It assumes that measurements are linear combinations of the states, and all disturbances are Gaussian. The influence diagram, a decision analysis tool that provides an algorithm for discrete-time filtering equivalent to the Kalman filter when the influence diagram represents Gaussian random variables, is discussed. The influence diagram algorithm is a factored form of the Kalman filter, similar to other factored forms such as the U-D filter. Compared with the Kalman filter, it offers improved numerical properties. Compared with other factored forms, it offers a reduced computational load 相似文献
243.
Li F. Liu H. Vaccaro R.J. 《IEEE transactions on aerospace and electronic systems》1993,29(4):1170-1184
Subspace based direction-of-arrival (DOA) estimation has motivated many performance studies, but limitations such as the assumption of an infinite amount of data and analysis of individual algorithms generally exist in these performance studies. The authors have previously proposed a unified performance analysis based on a finite amount of data and achieved a tractable expression for the mean-squared DOA estimation error for the multiple signal classification (MUSIC). Min-Norm, estimation of signal parameters using rotational invariance techniques (ESPRIT), and state-space realization algorithms. However, this expression uses the singular values and vectors of a data matrix, which are obtained by the highly nonlinear transformation of the singular value decomposition (SVD). Thus the effects of the original data parameters such as numbers of sensors and snapshots, source coherence and separations were not explicitly analyzed. The authors unify and simplify this previous result and derive a unified expression based on the original data parameters. They analytically observe the effects of these parameters on the estimation error 相似文献
244.
Viswanath H.C. Jones R.A. 《IEEE transactions on aerospace and electronic systems》1993,29(4):1195-1203
The anomaly in the displacement estimates obtained from a low-level Kalman-based average displacement estimator is used to detect multiple targets in a forward-looking infrared (FLIR) scene. The displacement estimates originating from the targets could be associated with the detected multiple targets and an updated estimated position of the target could be obtained. This procedure could be repeated for all targets in the scene to obtain multitarget tracking. The behavior of the expected value of the displacement estimates as a function of the number of iterations is investigated. The behavior of the displacement error covariance matrix and the Kalman gain matrix are discussed as functions of the number of iterations 相似文献
245.
Multiposition alignment of strapdown inertial navigation system 总被引:3,自引:0,他引:3
Lee J.G. Park C.G. Park H.W. 《IEEE transactions on aerospace and electronic systems》1993,29(4):1323-1328
The authors demonstrate that the stationary alignment of strapdown inertial navigation system (SDINS) can be improved by employing the multiposition/technique. Using an observability analysis, it is shown that an optimal two-position alignment not only satisfies complete observability conditions but also minimizes alignment errors. This is done by analytic rank testing of the stripped observability matrix and numerical calculation of the error covariance. It is also shown that an optimal three-position alignment accelerates the convergence of the alignment error compared with two-position alignment 相似文献
246.
The significance of external influences on the environment of Earth and its atmosphere has become evident during recent years.
Especially, on time scales of several hundred years, the cosmogenic isotope concentration during the Wolf-, Spoerer-, Maunder-
and Dalton-Minimum indicates an increased cosmic ray flux. Because these grand minima of solar activity coincide with cold
periods, a correlation of the Earth climate with the cosmic ray intensities is plausible. Any quantitative study of the effects
of energetic particles on the atmosphere and environment of the Earth must address their transport to Earth and their interactions
with the Earth’s atmosphere including their filtering by the terrestrial magnetosphere. The first problem is one of the fundamental
problems in modern cosmic ray astrophysics, and corresponding studies began in the 1960s based on Parker’s cosmic ray modulation
theory taking into account diffusion, convection, adiabatic deceleration, and (later) the drift of energetic particles in
the global heliospheric magnetic field. It is well established that all of these processes determining the modulation of cosmic
rays are depending on parameters that are varying with the solar magnetic cycle. Therefore, the galactic cosmic ray intensities
close to Earth is the result of a complex modulation of the interstellar galactic spectrum within the heliosphere. The modern
view of this cosmic ray modulation is summarized in our contribution. 相似文献
247.
Energetic particle observations in the interplanetary medium provide fundamental information about the origin, development
and structure of coronal mass ejections. This paper reviews the status of our understanding of the ways in which particles
are energised at the Sun in association with CMEs. This understanding will remain incomplete until the relationship between
CMEs and flares is determined and we know the topology of the associated magnetic fields. The paper also discusses the characteristics
of interplanetary CMEs that may be probed using particle observations. 相似文献
248.
N. Gopalswamy Z. Mikić D. Maia D. Alexander H. Cremades P. Kaufmann D. Tripathi Y.-M. Wang 《Space Science Reviews》2006,123(1-3):303-339
The coronal mass ejection (CME) phenomenon occurs in closed magnetic field regions on the Sun such as active regions, filament regions, transequatorial interconnection regions, and complexes involving a combination of these. This chapter describes the current knowledge on these closed field structures and how they lead to CMEs. After describing the specific magnetic structures observed in the CME source region, we compare the substructures of CMEs to what is observed before eruption. Evolution of the closed magnetic structures in response to various photospheric motions over different time scales (convection, differential rotation, meridional circulation) somehow leads to the eruption. We describe this pre-eruption evolution and attempt to link them to the observed features of CMEs. Small-scale energetic signatures in the form of electron acceleration (signified by nonthermal radio bursts at metric wavelengths) and plasma heating (observed as compact soft X-ray brightening) may be indicative of impending CMEs. We survey these pre-eruptive energy releases using observations taken before and during the eruption of several CMEs. Finally, we discuss how the observations can be converted into useful inputs to numerical models that can describe the CME initiation. 相似文献
249.
Jessica M. Sunshine Michael F. A’Hearn Olivier Groussin Lucy A. McFadden Kenneth P. Klaasen Peter H. Schultz Carey M. Lisse 《Space Science Reviews》2005,117(1-2):269-295
The science payload on the Deep Impact mission includes a 1.05–4.8 μm infrared spectrometer with a spectral resolution ranging
from R∼200–900. The Deep Impact IR spectrometer was designed to optimize, within engineering and cost constraints, observations
of the dust, gas, and nucleus of 9P/Tempel 1. The wavelength range includes absorption and emission features from ices, silicates,
organics, and many gases that are known to be, or anticipated to be, present on comets. The expected data will provide measurements
at previously unseen spatial resolution before, during, and after our cratering experiment at the comet 9P/Tempel 1. This
article explores the unique aspects of the Deep Impact IR spectrometer experiment, presents a range of expectations for spectral
data of 9P/Tempel 1, and summarizes the specific science objectives at each phase of the mission. 相似文献
250.