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681.
Kwa-Sur Tam Lifeng Yang Dravid N. 《IEEE transactions on aerospace and electronic systems》1994,30(3):800-808
To facilitate protection system studies on the space station electric power system, there is a need to develop a model that can accurately and conveniently simulate both the power system and the protection system. Models for two major protective devices, the remote bus isolator and the remote power controller, are described. These models have been installed in a power system model resembling one channel of the space station power system. The usefulness of these models in protection system studies Is demonstrated 相似文献
682.
N. N. Inozemtsev 《Russian Aeronautics (Iz VUZ)》2010,53(4):443-449
A problem of applying closed multiloop thermodynamic cycles with mixing of dissimilar working gases in spacecraft power plants has been considered. The advantage of these cycles that is due to reduction of a heat quantity being rejected into space has been shown for ecologically clean generation of electric energy in prolonged space flights. 相似文献
683.
Bershad N.J. Merryman P. Sklansky J. 《IEEE transactions on aerospace and electronic systems》1974,(2):245-254
The theory of ?continuous learning? is applied here to the design of nonlinear sampled-data trackers. This theory provides a continuous-motion approximation of the discrete or sampled motion of the actual tracker. The theory prodicts the transient-response performance of the tracker as well as the mean-square errors caused by noise and statistical fluctuations in the signal. Numerical examples of first-order and second-order trackers designed by this technique are presented. These examples illustrate the adaptive behavior predicted by the technique. In one of these examples the trade-off between transient-response performance and the suppression of noise-induced tracking errors is demonstrated. 相似文献
684.
Polychronopoulos G. Tsitsiklis J.N. 《IEEE transactions on aerospace and electronic systems》1990,26(2):282-292
A decentralized detection problem is considered in which a number of identical sensors transmit a finite-valued function of their observations to a fusion center which makes a final decision on one of M alternative hypotheses. The authors consider the case in which the number of sensors is large, and they derive (asymptotically) optimal rules for determining the messages of the sensors when the observations are generated from a simple and symmetrical set of discrete distributions. They also consider the tradeoff between the number of sensors and the communication rate of each sensor when there is a constraint on the total communication rate from the sensors to the fusion center. The results suggest that it is preferable to have several independent sensors transmitting low-rate (coarse) information instead of a few sensors transmitting high-rate (very detailed) information. They also suggest that an M -ary hypothesis testing problem can be viewed as a collection of M (M -1)/2 binary hypothesis testing problems. From this point of view the most useful messages (decision rules) are those that provide information to the fusion center that is relevant to the largest possible numbers of these binary hypothesis testing problems 相似文献
685.
A major challenge posed by aircraft tracking problems is the nondeterministic nature of an aircraft flight, due to the difficulty of predicting the pilot's actions. Accurate aircraft maneuver models are however highly desirable, particularly in air defense applications, to achieve accurate tracking and prediction. Through analysis of actual fighter aircraft trajectories and comparison with the Singer maneuver model, particularly in terms of prediction performance, coordinated turn (CT) aircraft maneuver models are presented, compared, and validated. A more general CT model is shown to better model actual trajectories than the classical CT model used in the literature 相似文献
686.
687.
Summary Photometric observations of A0538-66 in quiescence show that the optical star is an object of equivalent spectral type B7eII. Spectroscopic data taken simultaneously confirm this spectral classification and are consistent with the reported periodic variations seen in the emission lines. It is unlikely that the optical outburst is due to X-rays reprocessed in the atmosphere of the primary star or elsewhere. 相似文献
688.
N. N. Makarov 《Russian Aeronautics (Iz VUZ)》2007,50(4):415-421
The initial statements are formulated and a technique is considered to solve a problem of providing trouble-free airborne ergatic complex (AEC) operation under the action of external disturbances, equipment failure, pilot’s errors and other unfavorable factors. 相似文献
689.
R. N. Faizutdinov I. O. Spiridonov A. A. Baloev S. M. Chernyavskii 《Russian Aeronautics (Iz VUZ)》2017,60(4):551-558
A technique of multiobjective parametric design of line-of-sight stabilization system for an airborne electro-optical device is developed. The multiobjective design of the PI controller for the stabilization system being considered is performed. 相似文献
690.
I. N. Khaimovich 《Russian Aeronautics (Iz VUZ)》2014,57(2):169-174
The computer-aided design (CAD) system is specified for the preproduction engineering of the aircraft engine compressor blades. This system is characterized by a high quality of designing the finishing cutoff and reducing dies. It is shown that a high level of unification and integration in CAD permits the time of designing the punch tool sets to be significantly reduced. 相似文献