Olympus Mons Corporation
ECE 6390 - Fall 2008

Communications

Note: An extensive analysis of the communication systems, including plots, detailed simulations, and references, can be found in pdf form. A summary appears below:

Overview

The distance between Earth and Mars varies widely depending on the orbital position of each planet. Our goal is to maintain a data rate of at least 1 Mbps at the greatest Earth-Mars distance, which is approximately 401 million kilometers. Within the overall fleet of 18 active satellites, each constellation of 6 will contain one "master" satellite with a large Ka-band dish to communicate with Earth.

Deep Space Network

There are three Deep Space Network complexes around the globe, each equipped with a 70m dish antenna and several smaller 34m and 26m antennas. They are located at:

To support NASA's Mars Reconnaissance Orbiter, launched in 2005, several changes were made to the Deep Space Network. It now supports operation in the Ka-band, transmitting around 34.2 GHz and receiving at 32 GHz. Transmit power can reach 400 kilowatts. Using the Ka-band (as opposed to X-band, for example) allows for higher gain and bandwidth, with the trade-off being more disruption due to Earth's weather.

Turbo-coding

Beginning in 2003 the Consultative Committee on Space Data Systems (CCSCS) implemented Turbo Codes compatible with the Deep Space Network. Such codes can dramatically improve error correction methods used in the past, and are relatively easy to implement in hardware or software onboard our satellites. Using a (255;223) Reed-Solomon code with (rate-0.4998, length-8920) Turbo Codes will provide a final bit error rate of 10^-5 given a 1dB SNR.

Uplink Budget

Selected values are included here. For full details, view the pdf report.

Specification
Value
Notes
Frequency
34.45 GHz
Ka-band, compatible with DSN
Actual bit rate
1 Mbps
Physical bit rate
2.287 Mbps
Modulation
BPSK
Bandwidth
3.43 MHz
Physical Noise Temp
40 K
Satellite Antenna Gain
59.7 dB
Satellite Antenna Diameter
3m
Transmit Power
50 dBW
Maximum Distance
401 billion km
Received Power
-106.5 dBW
CNR
40.7 dB

Downlink Budget

Selected values are included here. For full details, view the pdf report.

Specification
Value
Notes
Frequency
32.05 GHz
Ka-band, compatible with DSN
Actual bit rate
1 Mbps
Physical bit rate
2.287 Mbps
Modulation
BPSK
Bandwidth
3.43 MHz
Physical Noise Temp
28 K
Satellite Antenna Gain
59.7 dB
Satellite Antenna Diameter
3m
Transmit Power
18 dBW
(63 watts)
Maximum Distance
401 billion km
Received Power
-138.5 dBW
CNR
3.64 dB

Mars-Orbit to Mars-Surface Link

The positioning signal transmitted from satellites in Mars orbit to positioning devices on the planet's surface is centered at 2.23 GHz and is constructed with Gold codes of length 2^13 - 1 = 8191. The autocorrelation of this code is nearly perfect. Processing gain is 39.1 dB. A series of simulations was performed in SIMULINK/MATLAB to evaluate the performance of the positioning system, and full details are provided in the pdf report. As an example, the simulation setup and results for the autocorrelation are shown below:

Using a system of 18 active satellites divided into 3 constellations allows for a maximum of 8 visible satellites at any one time. With an altitude of 17,708 km and transmit power of 4.92 dBW (3.1 W), the average received power on the ground is -172.22 dBW per satellite.

Our signal contains a 50 bps data signal riding on top of the positioning signal, just like Earth-based GPS. The coarse acquisition signal has a chip rate of 8191 x 50 = 409,550 chips/sec.

Spread carrier-to-noise ratio is -26.4 dB, which increases to 12.77 dB after despreading. After removing 1 dB for link margin, our estimated BER is an excellent 2.07E-8. At 50 bit/sec this represents 1 error in 11 days.

A full Simulink simulation of the GPS system can be downloaded here.

Satellite to Satellite Link

The master satellite in each constellation can act as a relay for signals from Earth. It will receive the high data rate signal with its large Ka-band antenna and relay a down-converted X-band signal to the satellites nearby when necessary, or use that transmitter to send other specific instructions as directed by Earth. This system will transmit with a 60cm dish antenna that broadcasts 5 dBW of power at 8 GHz.