Authors: John Harding, John K. Pollard, Leonore Katz-Rhoads, Peter Mengert, Robert Disarlo, E. Donald Sussman
Date of Publication: March 1999
Sponsoring Agency: U.S. Department of Transportation - Federal Railroad Administration
Performing Organization: USDOT Volpe National Transportation Systems Center High Speed Guided Ground Transportation Safety Task Force
Report No:
Abstract:
Proposed high-speed ground transportation systems, such as Maglev, may
have motion
characteristics affecting passenger comfort that set them apart from
anything previously
experienced. Operating at aircraft speeds along rights-of-way established
for conventional ground
vehicles, these systems may subject passengers to significantly larger
vertical accelerations and roll
rates than they have ever felt on existing common-carrier modes. If
the design limits for guideway
curvature are set too high in the interest of achieving the shortest
travel times and/or maximum
utilization of existing, short-radius right-of-way, substantial numbers
of passengers may find the
ride quality unacceptable because of excessive vertical acceleration
and roll rates. In that case,
speed would be reduced, resulting in moderately longer trip times.
In areas where new right-of-way
is unavailable, the question becomes how can a Maglev or other high-speed-system
guideway be
optimally fitted to it and what speeds should be used.
Previous research carried out by the Volpe National Transportation Systems
Center for the National
Maglev Initiative demonstrated that more than 95% of the public would
accept isolated Maglev
maneuvers involving bank angles up to 37 degrees and roll rates up
to 7 degrees/sec. Since these
limits were higher than those contemplated in most Maglev-system-design
proposals, passenger
acceptance did not appear to impose any significant constraints. However,
further reflection on
motion sickness as experienced in other modes suggests that the frequency
of occurrence of
motions, as well as their power spectra, are as important as their
magnitude and that the view out
the window may strongly influence the passenger’s likelihood of becoming
ill. Hence this study
was undertaken to explore comfort and motion-sickness effects of Maglev
travel in corridors
characterized by frequent curves.
Four segments of the New York State Thruway, totaling 277 km (172 miles),
were chosen as the
hypothetical route for evaluating passenger acceptance for the following
reasons:
To facilitate both the experimental design process and subsequent data
analysis, a procedure was
developed for estimating the propensity of a given set of ride motions
to induce motion sickness.
This procedure is based upon the work of M. J. Griffin and British
Standard 6841:1987 for ride
quality. It generates a number called the Motion Sickness Dosage Value
(MSDV), from which the
proportion of passengers who will experience nausea can be estimated.
The model predicts the
incidence of kinetosis from the magnitude and duration of exposure
to low-frequency (0.1 - 0.5 Hz)
vertical accelerations. For the hypothetical route, 27 alternative
sets of design limits for bank angle,
roll rate and longitudinal acceleration and deceleration were initially
considered, which had MSDV
scores ranging from less than 2 to 13. British Standard 6841 provides
an approximate method for
convenient interpretation of these figures. In a “mixed population
of unadapted male and female
adults” BS 6841 gives the estimate:
Percentage of persons who may vomit = 1/3 * MSDV.
Also, the scores may be used for comparative purposes; motions leading
to high MSDV scores may
be expected to produce more motion sickness than motions leading to
low scores.
The only means of simulating trips with realistic accelerations at
reasonable cost is through the use
of an airplane. In turning, aircraft naturally bank at just the right
angle to eliminate lateral forces on
the passenger, just as a Maglev would. Conventional ground vehicles
would produce unpleasant
and unrealistic lateral accelerations in rounding turns at high speeds,
since they are restricted to low
amounts of super-elevation and generally lack tilt-body suspensions.
The principal disadvantage of
using an airplane as a simulator is that it cannot provide a realistic
out-the-window view a future
Maglev passenger would see. Only a laboratory simulator can safely
expose passengers to the
visual effects of scenery rushing by at 400 kilometers per hour (about
250 miles per hour) at ground
level. The laboratory simulator can also add realistic amounts of vibration.
To provide facilities for testing subjects in both the airliner and
laboratory simulations, a contract
was awarded to Grumman Aerospace Inc. (now Northrop Grumman Corp.).
This contract
supported the development of computer-generated-imagery of the New
York State Thruway right-of-
way, use of the simulator and staff for testing subjects and use of
a 21-seat Gulfstream I and
crew for flight experiments. Due to the merger with Northrop and the
ensuing downsizing of the
corporate fleet, a Beechcraft 1900C replaced this aircraft.
An experimental apparatus was constructed to facilitate flying an airliner
through a series of several
dozen roll maneuvers which would subject passengers to the same vertical
accelerations and roll
rates they would experience in a Maglev built to a given set of design
standards. This apparatus
was based upon two notebook computers linked to a roll-rate gyro and
a three-axes accelerometer.
It generated a cockpit display showing what the aircraft’s bank angle
was supposed to be at any
given time, what its actual bank angle was, and the direction of the
next maneuver. The pilot’s job
was simply to keep the two bars on the display parallel. The apparatus
also recorded the outputs of
the accelerometers and rate gyro at 0.1-second intervals, thus allowing
MSDV
and other measures
of ride quality to be calculated.
After training the crew to fly the experimental procedures and securing
use of restricted airspace,
two preliminary tests were conducted using government and contractor
personnel as subjects.
These tests exposed subjects to two intervals of flying with relatively
high bank angle limits,
consistent with making the 277-km (172-mile) trip in about 38 minutes.
More than half the
subjects began feeling queasy at these higher limits. As a result,
a decision was reached to restrict
the exposure of subjects drawn from the general public to bank angles
of less than 30 degrees and
roll rates of less than 9 degrees/sec.
The final experimental design specified nine flights with 14 subjects
each. Each flight simulated a
277-km trip made with one of the nine possible combinations of limits
for bank angle and roll rate.
The limits for bank angle were 14, 21 and 28 degrees while those for
roll rate were 4, 6 and 8
degrees per second. Since the laboratory simulator seated only four
subjects, two sessions were
conducted with each combination of limits, allowing more than half
of the persons who had flown
to take the simulator trip as well. Subjects were required to rate
ride comfort and their own
tendency to motion sickness (both on seven-point scales) five times
during both trips and to read
magazine articles and answer questions about them.
Analysis of the data from the subject rating sheets and the instrumentation
lead to the following
conclusions:
No. of Pages: 100
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