Dj. Hewson et al., Aircraft control forces and EMG activity in a C-130 Hercules during strength-critical maneuvers, AVIAT SP EN, 72(3), 2001, pp. 165-169
Citations number
28
Categorie Soggetti
Envirnomentale Medicine & Public Health","Medical Research General Topics
Background: The force levels required to operate aircraft controls should b
e readily generated by pilots, without undue fatigue or exertion. However,
maximum pilot applied forces, as specified in aircraft design standards, we
re empirically derived from the subjective comments of test pilots, and may
not be applicable for the majority of pilots. Further, experienced RNZAF H
ercules flying instructors have indicated that endurance and fatigue are pr
oblems for Hercules pilots. The aim of this study was to quantify aircraft
control forces during emergency maneuvers in a Hercules aircraft and compar
e these forces with design standards. In addition, EMC data were recorded a
s an indicator of muscle fatigue during flight. Methods: Six subjects were
tested in a C-130 Hercules aircraft. The maneuvers performed were low-level
dynamic flight, one engine-off straight-and-level flight, and a two-engine
s-off simulated approach. The variables recorded were pilot-applied forces
and EMC activity. Results: Left rudder pedal force and vastus lateralis act
ivity were both significantly greater during engine-off maneuvers than duri
ng low-level dynamic flight (p < 0.05). Maximum aircraft control forces for
all controls were within 10% of the design standards. The mean EMC activit
y across all muscles and maneuvers was 26% MVC, with a peak of 61% MVC in v
astus lateralis during the two-engine-off approach. The median frequency of
the vastus lateralis EMG signal decreased 13.0% and 16.0% for the one engi
ne-off and two-engine-off maneuvers, respectively. Conclusion: The forces r
equired to fly a Hercules aircraft during emergency maneuvers are similar t
o the aircraft design standards. However, the levels of vastus lateralis mu
scle activation observed during the engine-off maneuvers can be sustained f
or approximately 1 min only. Thus, if two engines fail more than 1 min befo
re landing, pilots may have to alternate control of the aircraft to share t
he workload and enable the aircraft to land safely.