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start [2026/03/27 12:57] pkovarstart [2026/03/31 10:19] (current) pkovar
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-Tabbed Content 
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-''**[[start|pNav2]] • [[history|History]] • [[documentation|Documentation]] • [[about|About]]**'' 
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 ====== pNav2 - Pico Satellite GPS Receiver ====== ====== pNav2 - Pico Satellite GPS Receiver ======
  
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 ==== Features ==== ==== Features ====
 <columns 100% - -> <columns 100% - ->
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   * DSP acquisition unit for satellite acquiring acceleration   * DSP acquisition unit for satellite acquiring acceleration
   * Deduced reckoning when losing the GPS satellites   * Deduced reckoning when losing the GPS satellites
-  * Customizable output protocol+  * Customizable data exchange protocol
     * Extended NMEA protocol      * Extended NMEA protocol 
     * Easy to process binary protocol     * Easy to process binary protocol
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   * Evaluation software   * Evaluation software
   * Engineering model and Flight model licences   * Engineering model and Flight model licences
-  * Configurable NMEA and Binary messages 
   * Flight heritage   * Flight heritage
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-[[Documentation|Documentation]] 
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 <newcolumn> <newcolumn>
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 <figure> <figure>
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     * Patch antenna      * Patch antenna 
     * Antenna Cap     * Antenna Cap
-    * LAN+    * LNA
     * Test panel     * Test panel
   * Small dimensions   * Small dimensions
   * Low power consumption   * Low power consumption
-  * Now special knowledge for integration+  * No special knowledge for integration
  
 </columns> </columns>
  
-[[Documentation|Documentation]]+---- 
 + 
 +====== pNav2 Design Requirements ====== 
 + 
 +==== Original pNav Design Requirements ==== 
 +  * The CubeSat navigation receiver should be as simple as possible. 
 +  * It should integrate all necessary parts for navigation in the LEO Orbit 
 +  * It should be compatible with a 1U CubeSat platform, ie, power consumption should be a fraction of the power budget of 1U satellite. The receiver should be small and light.    
 +  * The applied signal and measurement processing algorithms should be simple and very robust 
 +==== + New Design Requirements ==== 
 +  * Rapid Cold Start and satellite reaqusition 
 +  * Continuous positioning of a rotating (unstabilized) 1U CubeSat 
 +  * Easy integration into the satellite
  
  
-#[[History|History]] [[Documentation|Documentation]] [[About|About]] 
  
start.1774612672.txt.gz · Last modified: by pkovar

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