An analysis of control reversal errors during unusual attitude recoveries using helmet-mounted display symbology
- PMID: 11846178
An analysis of control reversal errors during unusual attitude recoveries using helmet-mounted display symbology
Abstract
Background: Spatial disorientation (SD) refers to pilots' inability to accurately interpret the attitude of their aircraft with respect to Earth. Unfortunately, SD statistics have held constant for the past few decades, through the transition from the head-down attitude indicator (Al) to the head-up display (HUD) as the attitude instrument. The newest attitude-indicating device to find its way into military cockpits is the helmet-mounted display (HMD). HMDs were initially introduced into the cockpit to enhance target location and weapon-pointing, but there is currently an effort to make HMDs attitude reference displays so pilots need not go head-down to obtain attitude information. However, unintuitive information or inappropriate implementation of on-boresight attitude symbology on the HMD may contribute to the SD problem.
Objective: The occurrence of control reversal errors (CREs) during unusual attitude recovery tasks when using an HMD to provide attitude information was investigated. The effect of such errors was evaluated in terms of altitude changes during recovery and time to recover.
Methods: There were 12 pilot-subjects who completed 8 unusual attitude recovery tasks.
Results: Results showed that CREs did occur, and there was a significant negative effect of these errors on absolute altitude change, but not on total recovery time. Results failed to show a decrease in the number of CREs occurring when using the HMD as compared with data from other studies that used an Al or a HUD.
Conclusions: Results suggest that new HMD attitude symbology needs to be designed to help reduce CREs and, perhaps, SD incidences.
Comment in
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Control reversal using helmet-mounted displays.Aviat Space Environ Med. 2002 Sep;73(9):939; author reply 939-40. Aviat Space Environ Med. 2002. PMID: 12234051 No abstract available.
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