[ PROJECT: 001 ] [ MODE: DETAIL_VIEW ]

Fault-Tolerant Quadrotor Control

Jan 2026 to Present

ControlsAllocationMuJoCoCrazySim SITLROS2UAV

Max Roll Reduction

145° to 7.2°

Sim Conditions

24 validated

Allocation Methods

9 tested

System ArchitectureINTERACTIVE_DIAGRAM

Summary

Closed-form 3-motor allocation derived and validated for all 4 single-motor failure cases. Identified motor saturation as the root cause of attitude loss; a thrust clamp reduced max roll from 145° to 7.2° on hardware. MuJoCo rigid-body sim built for gyroscopic coupling, with sim-to-real validation across PID, INDI, and gyroscopic-compensation controllers.

allocator.pycode
# 3-motor allocation,
# motor 0 failed
W = clamp_thrust(
    M_3motor @ cmd_wrench
)

motor.set_pwm(
    [0.0, *W]
)
videocamProject Demo
VIDEO