Another critical aspect of the LTU-Rocket firmware is its state machine architecture. A rocket’s life cycle is linear but complex, moving through distinct phases: idle, armed, powered ascent, coast, apogee detection, and descent. The firmware manages these transitions with absolute authority. For instance, the detection of apogee—the point of maximum altitude—is a non-reversible event that triggers the deployment of recovery systems. The software logic must be unambiguous, utilizing multiple criteria (such as accelerometer zero-crossing and barometric pressure thresholds) to confirm this event. By strictly defining these states, the firmware prevents premature deployment during the high-dynamic-pressure phase of ascent or late deployment, which could result in ground impact damage.
git clone https://github.com/your-org/ltu-rocket-firmware cd ltu-rocket-firmware ltu-rocket firmware
What I evaluated
Another critical aspect of the LTU-Rocket firmware is its state machine architecture. A rocket’s life cycle is linear but complex, moving through distinct phases: idle, armed, powered ascent, coast, apogee detection, and descent. The firmware manages these transitions with absolute authority. For instance, the detection of apogee—the point of maximum altitude—is a non-reversible event that triggers the deployment of recovery systems. The software logic must be unambiguous, utilizing multiple criteria (such as accelerometer zero-crossing and barometric pressure thresholds) to confirm this event. By strictly defining these states, the firmware prevents premature deployment during the high-dynamic-pressure phase of ascent or late deployment, which could result in ground impact damage.
git clone https://github.com/your-org/ltu-rocket-firmware cd ltu-rocket-firmware
What I evaluated