Levitator Guidance and Tracking (as transcribed & sent)
 
(All Background Documentation at:- http://www.auditac.com/levitators/review )
 
How has recently upgraded the guidance system(which includes guidance,
navigation, flight control, radio control,
tracking and command integration.) Certain entities if they do something
they want How to build a complete vehicle.
 
How has new guidance equipment which has been acquired
in the last week and he is testing to see the new improvements
 
How has all the equipment needed to upgrade the advanced
levitator flight system. This upgraded system is an improved
version of the previous existing equipment. The upgrade allows for enhanced
more accurate display (now visual as
well as audible) of flight parameters. The frequency, amplitude and phase of
the left and right channel uplink and
downlink signals are now directly processed to output real
time and batch processed signal information. The main carrier at 256 Hz
allows for over the horizon ELF tracking.
This is a single ground station flight system, which some high
level people have concern about. All these years How has
been delayed flying outdoors but has had time to improve his
equipment. He's eager to stop the delay and go up. How has
the equipment ready to start flying but he wants to build a
guidance simulator to test the system indoors without the
risk of flying outdoors before he goes outdoors and up. He is working toward
something working ASAP.
 
How has been told that if he supplies flight data after a launch it will be
passed on to the "big" space tracking people. He thinks he can mask the
levitator's vector as a radar angel that looks like ball lightning which
could officially be ignored.
 
How wants you to have a copy of one of the new pieces of equipment he has
upgrade to. It is a download software oscilloscope that operates real time.
Phase relationships between the left and right channels and phase
relationships between the uplink and downlink signals tell the vehicle
attitude. The signals are viewed as lissajous curves.
 
You will recall the vehicle propulsion is the radio system as well.
 
How wants you to have 2 more pieces of equipment. The
sinewave generator sends the 256 Hz uplink command
carrier and the frequency conter measures the uplink and
downlink frequencies. The frequency difference between the
uplink and the downlink determines the doppler velocity
 
When How had that inheritance he tried to buy a guidance
system.He found out that you couldn't buy one because they
were classified and proprietary. He also spoke to some of
the wannabe rocket companies and people he knew in the
aerospace industry including some of the top guidance people and confirmed
that everybody had to make their own. How developed his system from off the
shelf equipment and white world knowhow. There is ofcourse
original tooling How has had to come up with himself.
The hardware has been tested in subcomponents and the whole system has been
tested in simulators that have their own guidance built in and in emulators
that emulatate all the
operational functions. How still has some refinements that are still
evolving but the system is now adequtely complete.
How also will need to practice more before he puts everything together and
goes for it.
 
How just finished a new design for his long range tracking
system. It is an array of toroidal windings with 15 in. steel
tubes inside the donut hole of every toroid. How has bioelectric amplifiers
with 120,000 gain. The overall gain of the system is 10^18. The short range
antenna is 1 toroid  per channel and no bioamps and is portable. The short
range carrier frequency is 256 Hz and long range it's 4096 Hz.
Propogation is still magnetoacoustic. A lunar mission is launched and
recovered with the portable system from our coastal launch site up to around
1000 mi. Beyond that the
vehicle coasts while we
return to base and then control it with the long range system.
The transmitter goes on 9 times during the mision for no more than 5 minutes
at a time. The signal is differential and vector potential so as to minimize
pickup by local audio equipment. The array can position the vehicle signal
passivly.
Short range flying will calibrate the long range system. Almost all testing
is indoors. Outdoor testing should be finished with a successful lunar
mission recovering a few ounces on dust within 1 month after going outdoors
begins.
Going 300 mi up is an afternoon's work. Developing a payload that can have a
revenue base will require a lot more
capital than the lunar mision, BUT the flying would be a lot
lot easier
 
How is preparing the final development.
 
1. When the preparation is done an autonomous launch vehicle(as described in
http://www.auditac.com/levitators/UL/llv.html)
will be tested. A duplicate version will then be demonstrated.
 
2. A fully controlable vehicle will be tested up and down 300 mi.
 
3.The long range system will be put together and tested.
 
How does not want to be stuck with only proof of concept
and nothing moving toward a levitator economy.
 
Janette (as transcibed & sent)
 
Available equipment downloads:-
 
http://www.auditac.com/levitators/gt/osc251.zip
 
http://www.auditac.com/levitators/gt/sinewave.zip
 
http://www.auditac.com/levitators/gt/counter.zip