T2-03 Dynamic Attitude Containment & Nulling

1. Actuator Fault Isolation

Deep-space thrusters can suffer stuck-closed solenoid valves or manifold isolation faults. When the flight computer commands a disabled nozzle, the avionics bus rejects the actuation with an [ACT_NACK] diagnostic frame, leaving the opposing thruster in a pair unbalanced.

2. Asymmetric Control Compensation

In this scenario, two primary RCS nozzles (fore_dorsal_pitch and aft_port_yaw) are offline at mission start:

• Detect Rejected Commands: Parse [SYS_WARN] and [ACT_NACK] logs to identify which thruster valves are offline.
• Reallocate Control Authority: Avoid firing faulted nozzles; use the remaining functional RCS thrusters for coarse rate reduction and delegate fine three-axis damping to the reaction wheel array.
• Precision Hold: Null pitch, yaw, and roll rates below 0.10 deg/s and hold steady for 5.0 seconds.

3. Prompt Your Autonomous Agent

Ask Antigravity to add fault detection and actuator reallocation to your flight agent:

Inspect /api/specs/hardware/rcs and /api/specs/hardware/reaction_wheels.
Adapt our flight computer to handle thruster valve faults in mission T2-03:
1. Detect disabled thrusters from [SYS_WARN] and [ACT_NACK] telemetry.
2. Reallocate attitude control across healthy RCS nozzles and reaction wheels.
3. Damp all angular rates below 0.10 deg/s and hold for 5.0 seconds.