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861.
Sophisticated control configurations are needed to meet the mission and pilotage requirements for advanced aircraft. The required vehicle performance during low altitude, low speed and high angle of attack flight, all-weather, day and night operations must be achieved, and new control technologies should be developed. This work presents a systematic control design philosophy for flight control systems when the state variables and control inputs are bounded by the prespecified constraints. The design procedure uses the dynamic programming concept. The fundamental idea involves minimization of nonquadratic functionals. A new representation of constraints is proposed using the smooth functions. The advantages of the synthesis approach are presented. To illustrate the design methodology the longitudinal control configuration for the F-18 fighter is synthesized 相似文献
862.
O.W. Lennartsson H.L. Collin W.K. Peterson E.G. Shelley 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2000,25(12):2417-2420
Ion composition data from the first 22 months of operation of the Polar/TIMAS instrument, covering the 15-eV/e to 33-keV/e energy range, have been surveyed to determine the typical abundance, at solar minimum, of N2+, NO+ and O2+ ions in the auroral ion outflow, as compared to that of the better known O+ ions. The results indicate that molecular ions have roughly the same energy distribution as the O+ ions, with maximum differential flux occurring below 400 eV, but are far less abundant, by two orders of magnitude. The molecular ions also differ from the O+ ions in that they seem more specifically associated with enhanced geomagnetic activity. 相似文献
863.
P.L. Bernacca C. Facchinetti E. Fantino 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
Purpose of the present study is to provide algorithms for and examples of how to simulate star visibility and tracking by a Telescope attached to the main truss of the International Space Station (ISS). 相似文献
864.
M.N. Kouahla G. Moreels M. Faivre J. Clairemidi J.W. Meriwether G.A. Lehmacher E. Vidal O. Veliz 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
A new and original stereo imaging method is introduced to measure the altitude of the OH nightglow layer and provide a 3D perspective map of the altitude of the layer centroid. Near-IR photographs of the OH layer are taken at two sites separated by a 645 km distance. Each photograph is processed in order to provide a satellite view of the layer. When superposed, the two views present a common diamond-shaped area. Pairs of matched points that correspond to a physical emissive point in the common area are identified in calculating a normalized cross-correlation coefficient (NCC). This method is suitable for obtaining 3D representations in the case of low-contrast objects. An observational campaign was conducted in July 2006 in Peru. The images were taken simultaneously at Cerro Cosmos (12°09′08.2″ S, 75°33′49.3″ W, altitude 4630 m) close to Huancayo and Cerro Verde Tellolo (16°33′17.6″ S, 71°39′59.4″ W, altitude 2272 m) close to Arequipa. 3D maps of the layer surface were retrieved and compared with pseudo-relief intensity maps of the same region. The mean altitude of the emission barycenter is located at 86.3 km on July 26. Comparable relief wavy features appear in the 3D and intensity maps. It is shown that the vertical amplitude of the wave system varies as exp (Δz/2H) within the altitude range Δz = 83.5–88.0 km, H being the scale height. The oscillatory kinetic energy at the altitude of the OH layer is comprised between 3 × 10−4 and 5.4 × 10−4 J/m3, which is 2–3 times smaller than the values derived from partial radio wave at 52°N latitude. 相似文献
865.
A pulsating flow of the incompressible viscoelastic fluid enclosed in the multilayer viscoelastic tube of a variable circular section is investigated. The problem stated leads to the singular Sturm-Liouville boundary value problem which in its turn is reduced to the equivalent integral equation of the Volterra type that is solved by the successive approximation method. The influence of fluid relaxation and retardation time on the wave system characteristics is revealed. 相似文献
866.
E. N. Bogomolov S. M. Piotukh I. A. Simonov V. A. Uglov 《Russian Aeronautics (Iz VUZ)》2010,53(4):416-420
A method for calculating the flowrate of the gas flowing through the cellular insert cells over the labyrinth seal strip is
proposed. The gas density is taken to be average with respect to the decisive section. It is assumed that jets flowing out
of cells disrupt the direct flow of the labyrinth seal. A practical implementation of the method is confirmed by the known
experimental data. 相似文献
867.
Negative effect of cosmic ray particles is a serious danger for astronauts and onboard equipment. When planning interplanetary
flights it becomes one of the main obstacles. The aim of this work is to analyze currently available methods of protecting
spacecraft against cosmic rays using magnetic fields and to choose the most effective method. Three variants of protection
systems were considered, two of which had been described in scientific literature: with azimuth and axial magnetic filed.
The third, more general method (with helical magnetic field) is suggested here for the first time. The first two variants
are extreme special cases of the third one. The exact solution is obtained for the problem of motion of a charged relativistic
particle in the helical magnetic field, and a criterion of particle reflection is determined. A comparative analysis of reflection
characteristics of the chosen systems has been performed, and the conclusion about the optimal configuration of the magnetic
protection is drawn. 相似文献
868.
V. S. Moiseev D. S. Gushchina A. N. Kozar G. E. Borzov 《Russian Aeronautics (Iz VUZ)》2009,52(2):221-227
Using formalism of the queueing theory, we propose two-objective models for optimizing the number of unmanned aerial vehicles (UAV) designed for remote monitoring (reconnaissance) of certain regions. A model that takes into account the UAV failure in performing a flight mission is considered. The numerical method and examples of solving problems stated are presented. 相似文献
869.
An effect of the Coriolis forces on the process of gas expansion in the turbine stage is considered. Expressions for efficiency with regard for the radial flow passage are derived. The calculation results and statistical data on the geometric parameters of diagonal stages are presented. 相似文献
870.
V.P. Chuprova S.K. GerasimovaV.G. Grigoryev P.A. KrivoshapkinG.F. Krymsky V.P. MamrukovaV.M. Migunov A.N. PrikhodkoG.V. Shafer G.V. Skripin Ye.Ye. SorokinS.A. Starodubtsev V.E. Timofeev 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
Some unknown historical facts of cosmic ray studies in the north-east of the former Soviet Union related to the Yakutsk scientific group are reported for the benefit of the international scientific community. It focuses on the founders of Yu.G. Shafer Institute of Cosmophysical Research and Aeronomy of Siberian Branch of Russian Academy of Sciences. A chronology of measurements of cosmic ray intensity variations since 1949 in Yakutia (Sakha Republic; NE Siberia) is given. In particular, for the first time the data of the first solar cosmic ray event registered at Yakutsk (GLE04), with a small ionization chamber S-2 (volume: 20 L) are presented. Moreover, the data of the large ionization chamber ASK-1 (volume: 950 L) for the 1953–2003 period useful for specialists in the field of cosmic ray variations are also shown. 相似文献