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ACTUAL PROBLEMS OF AVIATION AND AEROSPACE SYSTEMS
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Modelling of microaccelerations

with using of Weierstrass-Mandelbrot function

А.V.Sedelnikov

The microaccelerations problem having arisen in 1975 still has no cardinal solution. It is being got used to and now there is no such uncompromising struggle as at an initial stage of its development. Space technologies gave a powerful pulse to manufacture of ultra pure semiconductors, unique medicines, etc. But a real revolution in manufacture was not successful - those  microaccelerations  interfered which had an absolute value of less than 10-6g and were completely unperceptive for humans.

A number of researches believed that gravitational and aerodynamic accelerations were the basic contributors of microaccelerations and offered their estimations of these contributions to the total microacceleration level. However, these researches were mainly of theoretical interest. There is rather effective way of struggle against this part of microaccelerations. It is launching the space vehicle (SV) into high orbit where the gravitational and aerodynamic forces can be neglected.

Other microaccelerations caused by internal factors can not be treated like this. For example, for the process of growing the crystals with perfect structure it is necessary to maintain certain temperature that can deviate only by several hundredths of degree during three months. Overcooling or overheating the solution (or melt) is not allowed when SV respectively gets into Earth shadow or is exposed to the Sun light.

The problem of supplying SV with electric power was solved long ago by mounting the solar arrays (SA). SA operate efficiently being directed towards the Sun which is implemented by active SV orientation with help of the engines of position control system (EPCS). Here the most difficult and almost unsolvable problem occurs: microaccelerations arise of the order of 10-3 m/s2. This has a pernicious effect on complicated and subtle technological processes. For example, in case of crystallization the microacceleration growth leads to enhancement of convective movements which result in increase of capture of impurity and crystallization centers. Ordinary polycrystalline structure is obtained instead of perfect internal structure almost without weak intercrystalline bonds.

The start of EPCS excites the oscillations of SA that represent elastic and rather long structures (up to 7 meters). These oscillations (especially the most dangerous one - quasi-static component) do not decay up to the next EPCS start. The quasi-static microacceleration component is dumped very weakly. Therefore this is the subject of this paper and the majority of works on this considered research area.

One  should also note that the  apparatus for  measuring  microaccelerations of the order of 10-6g  are the ultra sensitive ones. The g-forces which they undergo at the SV start may most probably cause their fault. For example, there are the estimations of microaccelerations obtained with French accelerometers BETA. Their data on microaccelerations along three coordinate axes differed more than 20 times though there were no objective reasons. Perhaps, this was the case when apparatus failed to sustain the start g-forces.

Similar case of approximately 20-fold discrepancy of microaccelerations possibly takes place during the experiments on board of "Freedom" with vibration-isolating device MGIM. Researchers divided all the experimental series into successful and unsuccessful. Oscillation amplitude in the series also differed approximately 20 times. In this case the obvious objective reasons were also not detected. The project ended without results.

A number of researches believe that there is some objective unreliability of full-scale results related to microaccelerations.

Construction of adequate mathematical models of modern SV motion is rather complicated and laborious problem. Many changes, i.e. possible SV orbit, flight modes, etc., demand construction of new models taking into account some other disturbing factors. Thus, in the majority of modern models the microaccelerations are estimated after SV launch.

The problem of microaccelerations estimation at design stage before SV creation is still unsolved making the technological projects suffer. For example, the project of SV "Nika-T" was aimed at technological experiments but was not implemented (the author participated in construction of mathematical model for microaccelerations on board of SV). There is an objective need in microaccelerations estimation at the stage of SV design without any additional modeling. The problem is how to construct a statistical estimation of microacceleration level in the domain of supposed mounting of technological equipment without SV motion analysis. This estimation can help to solve some of the accumulated problems. This paper offers to obtain these estimations using the real part of Weierstrass-Mandelbrot fractal function (WMF).



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