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991.
V. S. Moiseev D. S. Gushchina A. N. Kozar G. E. Borzov 《Russian Aeronautics (Iz VUZ)》2009,52(3):372-375
We propose a mathematical model and the numerical method for an optimal choice of unmanned aerial vehicles (UAVs) from those
being in flight to fulfill a newly received order for monitoring (reconnaissance) of a new region. Examples of using the approach
being proposed and main lines of its realization in promising information unmanned aircraft complexes (UAC) are presented. 相似文献
992.
S. A. Mikhailov A. Yu. Onushkin Yu. P. Onushkin A. A. Safonov S. I. Kochish 《Russian Aeronautics (Iz VUZ)》2009,52(3):296-301
The algorithms for calculating available overloads and maneuvers are presented. Nesterov’s loop maneuver is analyzed. 相似文献
993.
With allowance made for thermoelasticity of working surfaces and inertia forces on the lubricant coat, a hydrodynamic problem
is solved for the noncontacting face seals with microgrooves in the high-speed rotors of FV engines. Also shown are the initiation
of surface waviness in the zone of lubricant coat fracture and the influence of its amplitude upon the seal characteristics. 相似文献
994.
V. A. Olaev 《Russian Aeronautics (Iz VUZ)》2009,52(1):88-93
A technique for the parametric synthesis of the navigation system on the basis of the magneto-inertial course transmitter is proposed; the technique makes it possible to minimize the error scatter in determining the ground speed components, to analyze a nature of the error scatter variation in determining the location coordinates in time, to simulate and further choose regular intervals of using additional data obtained from the radionavigational satellite system. 相似文献
995.
It is proposed that curves of metal creep be approximated by the time-relative linear law with the initial creep strain discontinuity; as a result, the solution of initial boundary value rheological problems is considerably simplified and is characterized by the adequate precision with a large service life. The labor intensity of computations is similar to the steady-state creep law. The introduction of functional material constants makes it possible to perform calculations of creep under the action of temperature that is different from the specified one in the basic experiments as well as calculations of nonuniformly heated structure elements. 相似文献
996.
Behnam H. Beheshti Fabian Wittmer Reza S. Abhari 《Aerospace Science and Technology》2009,13(8):450-458
The work presented investigates the aerodynamic drag and flow physics of an airship configuration. The investigation is carried out experimentally in a water towing tank. The purpose of this project is to improve the understanding of the aerodynamic characteristics of an airship through quantitative and qualitative approaches. Qualitative measurements of integral drag force and moment are measured in the presence of a crosswind. Flow visualization using colored and fluorescent dyes has been applied to improve knowledge of the aerodynamics of airship configurations with an emphasis on the boundary layer separation, transition and hull–appendage interference effects. 相似文献
997.
B.J. Lewis A.R. Green L.G.I. Bennett 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
In computer codes used to estimate the aircrew radiation exposure from galactic cosmic radiation, a quiet sun model is usually assumed. A revised computer code (PCAIRE ver. 8.0f) is used to calculate the impact of noisy sun conditions on aircrew radiation exposure. The revised code incorporates the effect of solar storm activity, which can perturb the geomagnetic field lines, altering cutoff rigidities and hence the shielding capability of the Earth’s magnetic field. The effect of typical solar storm conditions on aircrew radiation exposure is shown to be minimal justifying the usual assumptions. 相似文献
998.
The process of formation of a particles cloud (space debris) during breakdown of the Earth’s Artificial Satellite (EAS) is considered. A system of equations of motion is derived, and its analytical solution in the linear approximation for circular orbits is presented. The distinction between this solution and an exact numerical solution is indicated. The cases of satellite breakdown at the apogee and perigee on an elliptic orbit are also considered, and some characteristics of these processes are compared.__________Translated from Kosmicheskie Issledovaniya, Vol. 43, No. 4, 2005, pp. 269–273.Original Russian Text Copyright © 2005 by Gorelov, Zarubkin. 相似文献
999.
The regularities of propagation along the spacecraft-Martian surface-spacecraft path of a broadband Gaussian pulse in the condition of its dispersion distortions are considered in application to the problem of radiowave pulse sounding of the near-surface soil of Mars from onboard a satellite. The Martian night-side ionosphere reduces the energy considerably but does not lead to any distortion of the pulse envelope. At the sounding of a two-layer surface, the ionosphere influence, together with the signal absorption, manifests as the lower limit of the thickness of the upper layer reached for measurements in the scope of the planned experiment [1]. 相似文献
1000.
A technique for choosing a rational load-carrying scheme and weight analysis at the early stages of designing lifting surfaces with the use of a special model of the finite element method is proposed. The distribution of structure loads is determined with regard for its deformation. The numerical example is presented. 相似文献