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start [2026/10/09 12:20] – pkovarstart [2026/10/09 12:26] (current) – [+ New Design Requirements] pkovar
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 ==== Features ==== ==== Features ====
-  * GPS L1 C/A navigation receiver for CubeSats 
-  * Small size and low weight - compatible with 1U CubeSat 
-  * Low power consumption 
-  * Radiation-tolerant design -> long live in LEO 
-  * 15 channels 
-  * DSP acquisition unit for satellite acquiring acceleration 
-  * Deduced reckoning when losing the GPS satellites 
-  * Customizable data protocols 
-    * Extended NMEA protocol  
-    * Easy to process binary protocol 
-    * Earth-Centered Earth-Fixed position and velocity vectors 
-  * Easy to integrate antenna kit 
-  * Development kit 
-  * Evaluation software 
-  * Engineering model and Flight model licences 
-  * Flight heritage 
- 
- 
   * GPS L1 C/A navigation receiver for CubeSats   * GPS L1 C/A navigation receiver for CubeSats
   * Small size and low mass, compatible with 1U CubeSats   * Small size and low mass, compatible with 1U CubeSats
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   * Dead reckoning during GPS signal outages   * Dead reckoning during GPS signal outages
   * Customizable data protocols   * Customizable data protocols
-  * Extended NMEA protocol +     * Extended NMEA protocol 
-  * Easy-to-process binary protocol +     * Easy-to-process binary protocol 
-  * ECEF position and velocity vectors+     * ECEF position and velocity vectors
   * Easy-to-integrate antenna kit   * Easy-to-integrate antenna kit
   * Development kit available   * Development kit available
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   * Engineering Model and Flight Model licenses   * Engineering Model and Flight Model licenses
   * Flight heritage   * Flight heritage
- 
 <newcolumn> <newcolumn>
  
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 ==== Original pNav L1 Design Requirements ==== ==== Original pNav L1 Design Requirements ====
   * The CubeSat navigation receiver should be as simple as possible.   * The CubeSat navigation receiver should be as simple as possible.
-  * It should integrate all necessary parts for navigation in the LEO Orbit +  * It should integrate all necessary functions for navigation in Low Earth Orbit (LEO). 
-  * 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.    +  * It should be compatible with a 1U CubeSat platform, i.e., 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+  * The applied signal and measurement processing algorithms should be simple and very robust.
 ==== + New Design Requirements ==== ==== + New Design Requirements ====
-  * Rapid Cold Start and satellite reaqusition +  * Rapid cold start and satellite reacquisition 
-  * Continuous positioning of a rotating (unstabilized) 1U CubeSat+  * Continuous positioning of rotating, unstabilized 1U CubeSats
   * Easy integration into the satellite   * Easy integration into the satellite
  
  
  
start.1791541232.txt.gz · Last modified: by pkovar

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