http://www.lpi.usra.edu/meetings/lpsc1992/pdf/1135.pdf
The two body dynamics of an orbiting particle is usually governed by Newton's
laws of gravity and mechanics. Here the Kepler problem has been studied with the
addition of the Lorentz force of magnetism. For micrometeoroids and small man made
debris particles electromagnetic interactions may become important. The space
environment is filled with charged particles, electrons and ions, that may be deposited on
a 1 - 100 microns sized particle. The orbits of such charged particles have been
modeled in earth orbit, with the dipole magnetic field superposed on the gravity field.
An initial study of this problem has been conducted. Figures 1 illustrates a 600
second time frame of particles in a 300 kilometer altitude Earth orbit with a 5.7'
inclination. The solid line is the pure Kepler problem. The dashed lines are the paths
taken by various sized particles with a single positive charge of 1.6x10-'~ coulombs.
The additional energy required to deflect these particles from a Kepler orbit
comes from the deposition of charge at the initial stage in the calculation. From there
the energy of the particle is conserved since both the gravitational and magnetic forces
are conservative, i.e. $F d r = 0.
The orbit of 1 micron sized particles has been computed and the results a r e
shown in figures 2 through 5. The results of this numerical exercise in magneto-orbital
dynamics a r e rather unexpected, but appear physically correct when studied. The
particle was set in a 2000km orbit with a 5.7' inclination. Figure 2 displays how the
magnetic field torques the orbital plane. Figure 3 then shows how the orbit is flipped
over and shoved toward the north pole. This is analogous to the spin orbit interaction in
the quantum atom. He r e the magnetic moments of the Earth's magnetic field and the
orbit a r e parallel. The flip in the orbit is a result of the system's requirement to reach a
lower magnetic energy by antiorienting the magnetic moments. The energy lost by
reorienting the magnetic moment goes into gravitational potential energy by shoving the
orbit above the north pole.
Since this model is classical, and the electromagnetic radiation emitted by the
accelerating charge is negligible, events depart from the Bohr quantum analog above.
The charged particle finds itself in a magnetic bottle near the north pole, figure 4. The
spiralling charged particle is deflected upward by the converging magnetic field. The
spiral then climbs upward only to be drawn back down by gravity. The spiral bounces up
and down gradually reaching on average a lower altitude with each bounce. This
ephemeris run went for 84000 iterations, with three seconds per iteration, before the
particle crashed into the Earth. Figure 5 is a close up of the oscillating orbital spiral
shortly before it crashes into the earth.
This problem explores a hole in the current understanding of orbital mechanics of
particles. Ions and electrons in the Earth environment are treated as obeying the laws of
electromagnetism, and collectively according to plasma physics.
Saturday, January 28, 2012
Chapman Associates - 'MICRON' Miniature Command Radio System
http://www.minda.co.uk/micrn1.htm
Designed by Chapman Associates and manufactured in the U.K. by K-Tech Limited. | |||||||
![]() | Overview‘MICRON’ is a very small radio-controlled switching system, fully CAA approved for security use on aircraft, in which the miniature Radio-Switch has the capability to acknowledge automatically any valid commands received from an operator using a hand-held Command Unit. It operates at very low power in the licence-exempt UHF band, is battery powered, and all functions are managed by intelligent low-power microprocessors.Main features
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![]() | The Radio-SwitchThe Radio-Switch has no On/Off switch. When deployed, and using the battery economiser mode, the receiver is normally switched on for around 120 milliseconds every 2 seconds (i.e: a 6% duty-cycle) until a valid code is recognised, after which it then 'locks-on' and decodes the data received. This means, however, that any transmission from the Command Unit has to last for at least 2 seconds to ensure that it will be successfully 'captured' and decoded by the receiver.Once a valid transmission has been recognised by the Radio-Switch microprocessor, as soon as that transmission ceases the Radio-Switch changes to ‘transmit’ mode and an acknowledgement signal is sent. This comprises a short sequence of long or short tone ‘beeps’ which, when received by the Command Unit, inform the operator as to the new status of the output switch (ON or OFF). NOTE: The answer-back signal can be inhibited by removing the small RED jumper link.Following receipt of any valid command, the Radio-Switch stays ‘awake' for a further 10 seconds in case additional commands are to be sent. Any transmissions made during this period can be of quite short duration since the receiver is already 'awake'. Ten seconds after receiving the last valid transmission, the receiver reverts again to battery economiser mode. The Radio-Switch (if operating continuously) draws a current of around 4mA but, by using its battery economiser facility, this can be reduced to an average of around 250uA. If receiver battery power economy is not an important consideration and a faster response is required, the economiser can be completely disabled by fitting the YELLOW shorting-link. Visible indicators To enable the operation of the Radio-Switch to be easily monitored, three small LED’s are mounted on the PCB. They indicate the following:-
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![]() | The Command UnitThe Command Unit is housed in a black ABS case 146mm x 91mm x 34mm and powered by an internal 6 volt battery pack, comprising 4 x MN1500 (AA) batteries. It is designed to be hand-held and very simple to use. A quarter-wave whip antenna is attached to it by means of a BNC connector.On the front panel of the Command Unit is a rotary switch which provides On/Off switching and Identity selection of the Radio-Switch to be controlled. By pressing one of the two large push buttons, one Red and the other Black, the transmitter can be activated to send the appropriate ‘On’ or ‘Off’ command to the distant Radio-Switch. Whenever the transmitter is operating the two-colour LED at the top of the front-panel will light up red. As soon as the large push-button is released, the Command Unit’s receiver will be powered for a few seconds, the LED will change to green, and the acknowledgement from the Radio-Switch (if sent) should be heard on the built-in loudspeaker. Volume can be adjusted by means of a rotary control. In order to listen on the radio channel and check for possible interference, the receiver can also be switched on by holding down the small push-button adjacent to the Unit Identity selector switch. The LED will light up green when this is done also. When operating the Command Unit, if the LED fails to light, or is lit dimly when a button is pressed, the internal batteries probably need to be replaced. Even though the Command Unit has an On/Off switch (part of the Unit Identity switch), its quiescent current in ‘standby’ (not transmitting or receiving) mode is less than 150uA so, even if it was not switched off after use its battery drain is minimal. |
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