Samuel Low
🧠 🧠 🧠 **Future work:** to include single-satellite cases 🛰️ . The GUI should offer to the user the option of choosing single satellite processing (precise orbit determination) or dual...
⚠️⚠️⚠️ **Caution: Do not apply GPS antenna offsets as of v1.3 (pre-release).** ⚠️⚠️⚠️ GPS antenna offsets should be done in the spacecraft body frame. However, currently as LEOGPS has no...
🧠 🧠 🧠 **Future Work:** With the implementation of the coordinate frame transformation, tools are now available to perform both an orbit (ICRF) visualisation as well as a ground track...
🧠 🧠 🧠 **Future Work:** Inclusion of the processing statistics, such as pseudo range residuals, carrier to noise ratios, number of satellites in view, time series plot of which frequency...
Current LEOGPS basically performs pseudorange double differencing. Should eventually move towards carrier double differencing with IAR.
🏹 Goal: Figure out the extent of numerical integration errors using various tested numerical propagators. We attempt to investigate a numerical propagator that should be efficient (i.e. Runge-Kutta variants) but...