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201.
Space Science Reviews - 相似文献
202.
Some important regulation properties of satellite angular momentum dynamics are investigated using a combination of reaction jets and flywheels. The optimal feedback controller is designed in such a way that system regulation, under large perturbations, to a proper bounded subset in Rn, is achieved by using reaction jets. Thereafter, flywheels are activated to bring the system to the rest (desired) state. The domain and the size over which reaction jets are active, as well as the corresponding fuel cost, are discussed. Further, the effect of linear as well as nonlinear optimal feedback regulators on system behavior is indicated. Finally, the range (in the state space Rn) over which the flywheels are capable of regulating the system is also studied. 相似文献
203.
U. Geiser M. Sommer H. Haefner K.I. Itten 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1982,2(8):137-145
Heavy social and economic pressure on the available land resources in Sri Lanka are causing major land-cover changes. They need to be assessed to serve as input data for decision-making processes e.g. in agricultural or ecological planning.The Sri Lanka/Swiss Satellite Imagery Interpretation Project has developed a holistic approach to the mapping and monitoring of the land-use and the land-cover changes. The method applies intermediate level technology and is based on a benchmark/masking technique using satellite images, aerial photography and field surveys.The regular monitoring of changes of land-use types as a whole, e.g. forests, is part of the approach as well as the periodic assessment of changes within a specific land category, e.g. the seasonally cultivated riceland.The activities have to be transferred from the level of scientific research to the actual application within a reasonable time frame using the local resources. Discussed are also some of the problems inherent in the implementation of remote sensing activities in a so-called Third World country. 相似文献
204.
205.
The possibility of the existence of a trap mode in synchronous orbit is investigated. It is shown that when such a mode exists, certain parameters of the satellite orbit may soon attain undesired equilibrium values, thus complicating the normal stationkeeping operation of the spacecraft. A state-dependent control force which eliminates any such trap mode in the satellite orbit is then investigated. 相似文献
206.
This paper analyzes the operation of a phase-locked loop (PLL) preceded by a bandpass limiter (BPL) in the presence of impulsive noise. It is shown that the effect of the limiter consists essentially in a change of the statistics of the pulse strengths of the noise, so that the behavior of a BPL + PLL can be deduced from that of a simple PLL by suitable adjustment of the noise model. It is found that the limiter greatly enhances the PLL performance by reducing both the phase-error variance in the loop and the probability of cycle slippage. Finally, the design of the filter of the BPL is discussed, resulting in the conclusion that the best results are obtained by using a singletuned RLC circuit. 相似文献
207.
Pauluhn A. Solanki S.K. Schühle U. Wilhelm K. Lang J. Thompson W.T. Rüedi I. Hollandt J. Huber M.C.E. 《Space Science Reviews》2001,97(1-4):63-66
Space Science Reviews - Since the beginning of the SOHO (Solar and Heliospheric Observatory) mission an intercalibration programme was carried out which included simultaneous observations of the... 相似文献
208.
Bozzoni E. Marchetti G. Mengali U. Russo F. 《IEEE transactions on aerospace and electronic systems》1970,(2):249-252
The expression of the probability density function PClick(T) of the duration r of the clicks is determined as a function of 1) the expected number of clicks per second, Felick 2) the expected number of times per second that the noise component x(t) in phase with the carrier has instantaneous amplitude larger than that of the carrier itself 3) the probability density function peross(T) of the duration of the time intervals in which x(t) < -A 4) the probability that the values of the noise component in quadrature with the carrier will be of opposite sign at the extremes of time intervals of duration v. Using for Pcross(T) an approximate formula that holds fairly well in the range of the values of the signal-to-noise power ratio ? usually encountered, PIick(T) has been calculated for several values of a and for two shapes of the noise spectrum, Gaussian and rectangular. Finally, an expression is given for the mean value of T. 相似文献
209.
我国高能束流焊接技术经过半个世纪,特别是近20年的迅速发展,逐渐形成了自己的研发体系.国内众多研究者进行的一系列基础理论和应用研究为高能束流焊接技术的发展奠定了基础. 相似文献
210.
A. Francesconi C. Giacomuzzo A.M. Grande T. Mudric M. Zaccariotto E. Etemadi L. Di Landro U. Galvanetto 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
This paper discusses the impact behavior of a self-healing ionomeric polymer and compares its protection capability against space debris impacts to that of simple aluminium-alloy bumpers. To this end, 14 impact experiments on both ionomer and Al-7075-T6 thin plates with similar surface density were made with 1.5 mm aluminium spheres at velocity between 1 and 4 km/s. 相似文献