A resident maps the ADCS test matrix from sensor calibration to closed-loop fault recovery.
residents-ledger
test
adcs
matrix
desktop
Objective
unchanged
Confidence
heuristic
Margin
comfortable
1. The heist plan
The Quantum Thief is full of elaborate plans that depend on timing, misdirection, and knowing exactly where everyone is. An ADCS test matrix is a less glamorous heist: it schedules when each sensor will be checked, each actuator exercised, and each failure injected. The goal is to steal confidence from uncertainty.
2. Sensor tests
Test
Purpose
Key measurements
Star tracker calibration
Verify accuracy and noise
Pointing error, acquisition time, false stars
Stray-light rejection
Confirm operation with Earth/sun/moon outside FOV
Acquisition and hold under illumination
Sun sensor calibration
Verify FOV and accuracy
Angle error across field
Magnetometer calibration
Map sensor to known field
Residuals after hard/soft-iron compensation
Gyro characterization
Measure bias, scale factor, noise
Drift over temperature, ARW
GNSS timing and position
Verify position/velocity accuracy
Position fix latency and error
3. Actuator tests
Test
Purpose
Key measurements
Reaction wheel torque
Verify torque and momentum capacity
Torque linearity, friction, ripple
Wheel vibration
Check disturbance to payloads
Acceleration at wheel speed harmonics
Magnetorquer dipole
Verify torque in known field
Dipole moment, residual
Thruster torque coupling
Measure thrust-vector offset
Torque per firing, repeatability
4. Closed-loop and operational tests
Test
Purpose
Key measurements
Lost-in-space acquisition
Recover attitude from unknown state
Acquisition time, success rate
Pointing hold
Maintain each pointing mode
Pointing error, stability, power
Slew maneuver
Transition between targets
Slew time, settling, overshoot
Disturbance rejection
Recover from impulse torque
Settling time, peak error
Momentum dumping
Desaturate wheels
Time, propellant or power used
Sensor fault injection
Verify filter rejects bad data
Residuals, recovery time
Safe mode entry/exit
Confirm survival behavior
Sun acquisition, ground contact
ADCS-propulsion integration
Hold attitude during burn
Pointing error, momentum change
5. Test philosophy
Write the pointing-error budget and the fault-response requirements before the tests. A test that shows the platform can point to within 0.1 degree is only meaningful if the requirement is 0.1 degree or looser.