Back to Height Adjustment

Testing & Evaluation

V-Model Traceability: This page validates RM-5 (Provide ≥ 400 mm vertical stroke, full stroke ≤ 32 s) and RM-1 (Structural stability under punching loads), plus subsystem acceptance criteria HA-AC-1 (Actuator reliability under load) and HA-AC-2 (Delrin pad wear & backlash).

1. Performance Criteria

The height adjustment subsystem is evaluated against the following performance criteria, derived from the system-level requirements and specific actuation specifications:

ID Criterion Target
RM-5 Vertical stroke & speed ≥ 400 mm stroke completed in ≤ 32 s
RM-1 Structural stability Remain upright and maintain alignment under combined punch loads
HA-AC-1 Actuation reliability 5 consecutive full cycles under 60 kg payload without stalling
HA-AC-2 Delrin wear & backlash Pad wear < 1 mm, lateral backlash < 2 mm after 200 cycles

2. Test Procedures

Test 1: Stroke Length & Speed Test RM-5, HA-AC-1

Test 2: Structural Deflection under Punching Loads RM-1

Test 3: Delrin Wear & Backlash Endurance HA-AC-2

3. Results & Discussion

Test 1: Stroke Length & Speed Test RM-5, HA-AC-1

Results

The height adjustment stage achieved a maximum vertical stroke of 28 cm (accommodating a user height range of 150–178 cm, short of the 190 cm target) before being constrained by the internal cable length connecting the top and bottom electronics. The stroke descent was timed at 1 minute 26 seconds (86 s), which exceeded the 32-second target. This slower speed was due to utilizing an alternative motor rather than the originally specified screw-jack motor.

Video: Stroke Length & Speed Test showing the structure descending.
Discussion & Limitations

Test 2: Structural Deflection under Punching Loads RM-1

Results

At present, the height-adjustment subsystem has been validated structurally through load-path reasoning and empirical impact recording. The raw wireless IMU data was processed through a custom Python Digital Signal Processing (DSP) pipeline (using a 4th-order Butterworth low-pass filter with a 0.5 Hz cutoff) to isolate the true low-frequency structural sway from the high-frequency impact shockwaves and horizontal sliding artifacts.

Graph Interpretation: The DSP analysis (Figure below) illustrates the system's dynamic response to the 45-strike matrix. The Impact Vibration graph (left) captures the kinetic energy propagating through the frame. The distinct repeating pattern of "low, medium, high" clusters corresponds perfectly to the test procedure: the 5 light, 5 medium, and 5 hard punches were delivered sequentially to the Center pad, then repeated on the Right pad, and finally repeated on the Left pad. The Structural Sway graph (right) tracks the calculated angular deflection. While the top tube (Level 4) shows a controlled sway of around 3.5° under hard center impacts, the base (Level 1) occasionally exhibits massive spikes that exceed the top tube. As detailed in the Discussion below, these base spikes are not true angular tipping; rather, they are horizontal sliding artifacts caused by the base jolting and slipping on the floor, particularly when struck on the off-center (Right and Left) pads which introduce a sudden twisting moment.

Video: Physical demonstration of structural deflection and energy dissipation under medium to hard punching loads.
Discussion & Limitations

Upon rigorous mechanical engineering review, the DSP methodology utilized to derive the angular sway presents inherent limitations associated with accelerometer-based tilt calculations during dynamic impacts.

The analytical script calculated the absolute tilt angle by taking the arc-cosine of the dot product between the low-pass filtered instantaneous acceleration vector and the resting gravity baseline. This mathematical approach relies on the quasi-static assumption that the only low-frequency acceleration acting on the sensor is the 1g downward pull of gravity.

When subjected to a hard punch, the robot experiences violent lateral translational acceleration. Because accelerometers cannot distinguish between true angular tilt and horizontal acceleration (Einstein's equivalence principle), the initial raw data exhibited physically impossible >16° spikes at the base. These were horizontal sliding jolts misidentified as tilt.

While applying a strict 0.5 Hz Butterworth low-pass filter successfully eliminated these high-frequency sliding artifacts, a 0.5 Hz cutoff (representing a 2-second vibration period) is almost certainly below the natural resonant frequency of the steel cantilever column. As a result, the filter likely attenuated the true peak dynamic bending of the structure along with the noise. The 3.5° value recorded at the top tube should therefore be interpreted as a heavily damped, quasi-static deflection rather than the absolute instantaneous dynamic peak.

Recommendation: For future dynamic deflection testing, the true angular sway should be calculated by integrating the IMU's gyroscope data (angular velocity) over the brief impact window, fused with the accelerometer data via a Complementary or Kalman filter to correct for drift, making the calculation immune to horizontal sliding jolts.

Overall Structural Implications: Despite the instrumentation limitations in capturing the exact instantaneous peak deflection, the empirical test demonstrated the physical robustness of the height-adjustment assembly. While the structure exhibits noticeable transient vibrations and shaking under heavy impact, it remained upright throughout the extensive strike matrix without experiencing plastic deformation, tipping, or mechanical binding. This practically validates that the telescopic steel column and Delrin pad interfaces are effectively absorbing the overturning moments, shielding the internal screw-jack actuator from harmful lateral shear forces as intended by requirement RM-1.

Test 3: Delrin Wear & Backlash Endurance HA-AC-2

Results

Pending 200-cycle mechanical endurance test.

Discussion & Limitations

To be evaluated upon completion of the physical endurance test.

Overall Subsystem Assessment

ID Criterion Measured Result Status
RM-5 / HA-AC-1 Stroke & Reliability Vertical Stroke: 28 cm achieved (Target: 40 cm)
Stroke Duration: 1 min 26 s / 86 s (Target: ≤ 32 s)
User Height: 150–178 cm accommodated (Target: 150–190 cm)
Partial
RM-1 Structural deflection DSP analysis confirmed acceptable structural stability within operational limits. While visible shaking and vibration occur under impact, the peak quasi-static structural sway remained under 4° at the top of the steel tube (106.0 cm) during the hardest punching loads. Impact vibration data showed kinetic energy is safely dissipated down the column without causing base lift-off or permanent plastic deformation. Passed
HA-AC-2 Delrin wear & backlash Pending 200-cycle mechanical endurance test. Partial

4. Cross-References

Prev: Load Analysis Next: Padding Subsystem