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C00002 00002 COMPUTER CONTROLLED AIRPLANES
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COMPUTER CONTROLLED AIRPLANES
1. Introduction
Computers are already used in a number of military airplanes
and are projected for the supersonic transport. This article is
concerned with the use of computers in present planes even including
light planes. We envisage a small real time computer no larger than
a PDP-8I carrying out tasks in the areas of navigation, collision
avoidance and responding to traffic control, monitoring the condition
of the airplane, optimizing flight path taking into account fuel,
load, weather, and traffic.
2. Navigation
We advocate no basically new electronic navigation systems.
The basic system we consider is the familiar omnirange. However, the
computer will switch its radios at .1 second intervals among all
available omnis and will compute each few seconds a best estimate of
the current position of the aircraft. This estimate will be
displayed for the pilot on a map on a CRT and will be available for
interrogation from the ground or other airplanes. More accurate
positions should be available than at present because any systematic
inaccuracies in the radials of an omni due to terrain can be allowed
for by the computer; a correction equation for the omni will be
stored along with its position in the computer equivalent of the
sectional chart. Our goal is that navigation be accurate enough so
that aircraft can be flown close enough together so that there will
be enough airspace for everybody without danger of collision.
All instruments now available to the crew will be read by the
computer at appropriate intervals, e.g. every .1 to 10 seconds
depending on the instrument. In navigation, altitude, airspeed, and
heading information will be integrated with the information obtained
from the omnis. The amount of information available is much greater
than is required to monitor position, and any inconsistencies will be
detected and the offending instrument reported to the crew.
3. Collision avoidance and traffic control
Here again we want a system with large redundancy. The basisc
scheme is that the air traffic control computer interrogates each
airplane every few seconds and gets its position information or
perhaps even the raw bearing information received from the omnis.
Since the interrogation is electronic, a single 25kc band could
interrogate 100 airplanes per second at 250 bits per interrogation.
Each airplane can be given relevant traffic information or specific
collision avoidance instructions if this is desired.
In addition to the standard information transmitted to the
airplanes, special messages addressed to the crew of an airplane can
be presented on the CRT or printed on a strip printer.
Additional redundancy can be obtained by timing signals
returned from a plane or even signals transmitted from the ground to
a plane, then to another plane and then to another ground receiver.
4. Monitoring
The crew of an airplane is supposed to monitor all the
instruments at regular intervals. However, this activity can be done
much more reliably by a computer. Moreover, the computer can relate
such information as airspeed, attitude, engine RPM, fuel flow, and
air pressure and temperature and check continuously for fall off of
engine performance or ice buildup. Other parameters that can be
monitored include electrical system performance including
availability of emergency power, correct functioning of navigation
and other lights, icing conditions, navigation checkpoints,
maintenance of communication, and all engine instruments.
5. Visual monitoring
With the aid of television cameras, a computer can be
programmed to use visual information. The possibilities include
finding airports and runways under visual conditions, landing, taking
off, and taxiing, terrain avoidance, and collision avoidance. In
short, the computer can potentially perform the full range of chores
of the VFR pilot. All this, however, places much larger demands on
the computer and the programming than the previous applications and
is therefore somewhat further in the future.