Vertical Speed Indicator (VSI/IVSI): Principle, Lag, and Turning Error
The Vertical Speed Indicator (VSI) displays the rate of climb or descent in feet per minute (ft/min) or meters per second (m/s).
Principle of Operation
The VSI measures the rate of change of static pressure.
- Capsule: Connected directly to the static vent (pressure changes immediately).
- Case: Connected to the static vent through a restricted orifice called a metering unit (pressure changes slowly).
- Operation: During a climb, the pressure inside the capsule drops instantly, while the pressure in the case remains higher for a moment due to the restriction. This differential pressure causes the capsule to compress, indicating a climb.
Approximate Conversion: $1 \text{ m/s} \approx 200 \text{ ft/min}$.
Instantaneous VSI (IVSI)
Conventional VSIs suffer from lag (a delay of several seconds). The IVSI overcomes this using an accelerometer system (dashpots/pistons).
- Mechanism: When a climb/descent is initiated, the vertical acceleration moves a piston, creating an immediate pressure change in the capsule to drive the pointer before the static pressure differential builds up.
- Turning Error: In steep turns (bank > 40°), the accelerometer may react to G-forces, causing erroneous indications.
- Turbulence: IVSI can be over-sensitive in turbulence; pilots should scan trends rather than instantaneous fluctuations.
Blockage
Since the VSI relies solely on static pressure:
- Static Blockage: The pressure in the capsule will eventually equalize with the pressure in the case (trapped pressure). The instrument will fall to zero regardless of the aircraft's actual vertical motion.
- Pitot Blockage: No effect.