Satellite Systems

Acquisition, Processing, Storage and Communication with Power and animation

Defense and Space

  • Radar System
    Hardware-software mapping of a Radar system for a aircraft.
  • Software-Defined Radio
    Software Defined Radio with ADI9361 and ADI9371
  • Air-Ground Mission
     Network of satellites, aircrafts and ground stations
  • Satellite Modem
  • UAV
    Hardware architetcures
  • Jet Engine Controller
    Designing the controller
  • Satellite Systems
    Acquisition, Processing, Storage and Communication with Power and animation
  • Cubesat
    Implementation of a Air Force Cubesat model that can be used as a template to create any Cubesat architecture. Include support for battery, different activities per orbit and response times.

Animation_Target_Processing

Browsable image of the model.

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    macOS - Compatibility:macOS 10.15 (Catalina) or higher (*)
    Linux - Compatibility:Ubuntu 18.04 LTS or higher (*)
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  • Mouse over the icons to view parameters. Click on hierarchy and plotters to reveal content (if provided).
  • To simulate, click on Launch button, open downloaded file and click Run on the Java Security Page.
Animation_Target_Processingmodel <h2>Sun</h2><table border="1"><tr><td><b>Parameter</b></td><td><b>Expression</b></td><td><b>Value</b></td></tr><tr><td>Block_Documentation</td><td>Enter User Documentation Here</td><td>Enter User Documentation Here</td></tr><tr><td>Battery_Charge_Hr</td><td>Battery_Charge_Hr</td><td>1440.0</td></tr><tr><td>New_Charge</td><td>New_Charge</td><td>50</td></tr><tr><td>Variation</td><td>10</td><td>10</td></tr></table> <h2>Satellite</h2><table border="1"><tr><td><b>Parameter</b></td><td><b>Expression</b></td><td><b>Value</b></td></tr><tr><td>Block_Documentation</td><td>Enter User Documentation Here</td><td>Enter User Documentation Here</td></tr><tr><td>stepInRadians</td><td>PI/30.0</td><td>0.1047197551197</td></tr><tr><td>SimTime</td><td>SimTime</td><td>86401</td></tr><tr><td>Baseline_Battery</td><td>Battery_Charge_Hr * 0.1</td><td>144.0</td></tr><tr><td>SDRAM_Speed</td><td>600.0*SpeedFactor</td><td>360.0</td></tr><tr><td>Exec_Speed</td><td>600.0*SpeedFactor</td><td>360.0</td></tr><tr><td>SRAM_Speed</td><td>500.0*SpeedFactor</td><td>300.0</td></tr><tr><td>Bus_Speed</td><td>500.0*SpeedFactor</td><td>300.0</td></tr><tr><td>Link_Speed</td><td>500.0*SpeedFactor</td><td>300.0</td></tr><tr><td>Battery_Charge_Hr</td><td>Battery_Charge_Hr</td><td>1440.0</td></tr><tr><td>SpeedFactor</td><td>Technology_Selection</td><td>0.6</td></tr><tr><td>Low_Range</td><td>600.0</td><td>600.0</td></tr><tr><td>High_Range</td><td>900.0</td><td>900.0</td></tr><tr><td>SDRAM_Size</td><td>SDRAM_Size</td><td>8000</td></tr><tr><td>Next_Low_Range</td><td>8000.0</td><td>8000.0</td></tr><tr><td>Next_High_Range</td><td>9600.0</td><td>9600.0</td></tr></table>

The satellite is rotating around the earth. Inside the satellite there is a behavior and an architecture. There is also a power management module. When the satellite is on the side between the earth and Sun, the array panels are charging with the battery. When they are on the eclipse (or night) side, then there is only a discharge. When the satellite power reserve goes below a threshold, the model stops all processing. The processing is restarted when the satellite starts charging the battery again.

In the model, there are three stages- capture of the target images, process the images and transfer via downlink to the ground station. Each of these stages has different processing requirements. The acquisition and downlink can be performed only during target time periods.

There are a number of analysis being performance:

1. What is the system architecture configuration and speeds.
2. What should be the downlink speed?
3. How much is the power consumption?
4. How many targets can be acquired and processed.
5. What is the memory/storage requirements?
6. What is the array size i.e. what is the power charging rate required?