October 27-29, 2000 - Klofas.com

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!"'-------------fl>4OO_SIR:IU)_OI\Ioll£R--------------; I 1>3£ SPAa:CIWT , 1---r--9j)Q----; PJC ATTACH rtTTlNC -r=~=f===~ ..~-----_.,.__r , I I , i i i .j~ ~ Fig.2, Ariane 5 Space Available 9
10 Fig.3, P3E Line Overview
Page 1 and 2: jL 7££ $15.00 A MSAT RADIO AMATEU
Page 3 and 4: Copyright © 2000 by The American R
Page 5 and 6: Table of Contents (continued) APRS
Page 7 and 8: Welcome It is with great pleasure
Page 9 and 10: had characteristic perigee values o
Page 11 and 12: the digital experimenters will want
Page 13: Fig.1, P3E Rendered overvieW
Page 17 and 18: Amateur Radio On-board the Internat
Page 19 and 20: of "transportable stations" which c
Page 21 and 22: The packet bulletin board system on
Page 23 and 24: Side view of the EVA handrail ada
Page 25 and 26: wishing to review the status of the
Page 27 and 28: 2. CUBESAT DEVELOPMENT PROGRAM Aft
Page 29 and 30: The P-POD is constructed using 7075
Page 31 and 32: N 0"1 4 .3 2 NOTES: IN..ESS OTI£RW
Page 33 and 34: Payload services are designed to pr
Page 35 and 36: Assembly is simple. The RF circuit
Page 37 and 38: Level 2) To receive some beacons fr
Page 39 and 40: Amateur radio frequencies (and lice
Page 41 and 42: 2. These organizations could move t
Page 43 and 44: 5 "Space System Developments at Sta
Page 45 and 46: On 10450, it may not be enough to f
Page 47 and 48: Converters A converter converts one
Page 49 and 50: 44 falls offby 3 dB from the highes
Page 51 and 52: And higher still: S and C Bands Her
Page 53 and 54: Summary The higher bands on P3D off
Page 55 and 56: Mountaintop, P A 18707 (570) 868-56
Page 57 and 58: product using another media. Those
Page 59 and 60: Ground Track The unit vector (V LCH
Page 61 and 62: sin((J) = The velocity vector is th
Page 63 and 64: FIGURE 2 DEFAULT SETTINGS FOR A TIM
Page 65 and 66:
identified under the AMSAT Output F
Page 67 and 68:
The command and control mode VN dat
Page 69 and 70:
Most of the TNC-2 based TNCs have a
Page 71 and 72:
Ahstract Distributed Processing Goe
Page 73 and 74:
SETI@)home's power derives from cle
Page 75 and 76:
ARGUS@home won't happen overnight.
Page 77 and 78:
Figure 3: Graham Vincent, SEll Leag
Page 79 and 80:
o lola••ec("dmg1en'lth ~ 339 31
Page 81 and 82:
On AO-27 and UO-14 the downlink is
Page 83 and 84:
little planning even urban settings
Page 85 and 86:
A Spread Spectrum Wideband Transpon
Page 87 and 88:
nadir-pointing attribute of the Pal
Page 89 and 90:
signal, one to monitor the station'
Page 91 and 92:
Instanffune for the FT-IOO Anthony
Page 93 and 94:
The flIst problem is that you canno
Page 95 and 96:
Due to the way that the FT-IOO work
Page 97 and 98:
Auxiliary Receiver InstantTune lets
Page 99 and 100:
Similarly, the "itstart.bat" file i
Page 101 and 102:
Step 1 Quit from InstantTrack putti
Page 103 and 104:
Once you have turned on , control t
Page 105 and 106:
DOWN step DATA 1 3 Tuning Complete
Page 107 and 108:
EXAMPLES: 1. Change COM 3 to use IR
Page 109 and 110:
The name of the satellite must matc
Page 111 and 112:
eacon 29.4081 cw Auxiliary Fixed Tr
Page 113 and 114:
• Check to see that the COM port
Page 115 and 116:
Even with P3D in orbit and operatin
Page 117 and 118:
'atelllte :je:?lmJC!gNumbeet::'~ Ep
Page 119 and 120:
REFERENCES Specific technical infor
Page 121 and 122:
The potential of two-way satellite
Page 123 and 124:
Igates with operators that have vol
Page 125 and 126:
any time while also monitoring the
Page 127 and 128:
universal frequency where ALL APRS
Page 129 and 130:
DISTRIBUTING LIVE SAT TRACKING DATA
Page 131 and 132:
The Houston AMSAT Net I earned myHa
Page 133 and 134:
VNIW Real Audio Geostationary Comme
Page 135 and 136:
finnware (verses EPROM) and the EEP
Page 137 and 138:
Rotor Calibration First and foremos
Page 139 and 140:
Deadband Commanded Value ,/ For exa
Page 141 and 142:
of dissimilar radio models. For exa
Page 143 and 144:
Calibration Limits Command Meaning
Page 145 and 146:
and the T APR EasyTrakTM AzlEI Ro
Page 147 and 148:
Software Design If the world was fl
Page 149 and 150:
Rotor Control Window 1 (Normal Mode
Page 151 and 152:
Automatic Weather Balloon Tracking
Page 153 and 154:
148
Page 155 and 156:
Camera Tracking Recent events have
Page 157 and 158:
BEARING is only accurate if you are
Page 159 and 160:
Applications of PIC Microcontroller
Page 161 and 162:
TNC must simultaneously be in commu
Page 163 and 164:
This leads to the selection ofa mod
Page 165 and 166:
Distributed system for LEO satellit
Page 167 and 168:
a sender and a lot of receivers, po
Page 169 and 170:
Figure 2. Processes in the main app
Page 171 and 172:
The new G3RUH software modem for th
Page 173 and 174:
Figure 3. Multirate processing Figu
Page 175 and 176:
MODE-V/I EASY-SATS FOR EVERYONE Bo
Page 177 and 178:
usable downlinks across a 30 Khz ba
Page 179 and 180:
• First is the requirement for a
Page 181 and 182:
Thayer School of Engineering at Dar
Page 183 and 184:
mechanical support as well as the s
Page 185 and 186:
In tandem with data acquisition and
Page 187 and 188:
opportunities. Modularity by design
Page 189 and 190:
AMSAT SYMPOSIUM PRESENTATION PHASE
Page 191 and 192:
emember awaiting the sun to go down
Page 193 and 194:
communications, this will open up a
Page 195:
About the Author ... Dominick ''Dee
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October 27-29, 2000 - Klofas.com

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