PEGAS
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Powered Explicit Guidance Ascent System - a KSP & RO autopilot using the Space Shuttle guidance algorithm, UPFG
The vehicle definition (`vehicle`) is a static, user-input data structure unrelated to `sequence`, in which the user defines launch sequence events. In order to provide UPFG with complete information on...
In very specific circumstances PEGAS can fail to perform the final engine shutdown. Example of this behavior can be observed for a 2.5 stage vehicle where the last stage is...
Hey, updating from v1.2 to v1.3 for most of my rockets the g limiter disengages between fairing separation and burnout of the first stage. This happens to all rockets where...
As first observed in #47, RO engines sometimes take so long that the thrust watchdog mistakes this for a lack-of-thrust event and terminates the flight. This is however only the...
I have a second stage with `gLim` and `minThrottle` set to the appropriate values, but wherever the throttle reaches the minimum the engine just shuts down instead of holding that...