Computer graphics processing and selective visual display system – Image superposition by optical means – Plural image superposition
Reexamination Certificate
2002-09-10
2004-11-23
Eisen, Alexander (Department: 2674)
Computer graphics processing and selective visual display system
Image superposition by optical means
Plural image superposition
C345S629000
Reexamination Certificate
active
06822624
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to systems that generate signals for displaying graphic images and/or video images.
2. Description of the Related Art
Displays are part of many systems and are often used as instruments to provide graphical information to operators of the systems. The information displayed can, for example, represent the current status of a system or represent video, graphical and/or textual information that is used by an operator of the system to control and/or modify the operation of the system. In many applications, displays provide a plethora of textual information shown simultaneously at different locations on the displays. The observer would, in many such cases, typically consider several different items or pieces of textual information to properly determine the status of the system or to reach a conclusion about the particular matter being displayed. In yet other applications, displays may provide other graphical information simultaneously with the textual information to allow an observer or operator of the system to more quickly understand or reach a conclusion about the information being displayed. Displays are also used as a tool for various communication based systems such as personal computers, televisions receivers and security monitors where the displays receive signals from a remote or local (or both) signal source and provide the information to a user of the system. In some cases, the displays are providing graphical and/or video information where such information originate from different sources. Displays are implemented with various technologies to create display devices such as Cathode Ray Tube (CRT) monitors, Liquid Crystal Displays (LCD) and plasma displays.
One key application of displays is their use in monitoring, in real-time, various events and to provide a visual indication of such events in graphics form thus allowing an observer of such a display to make decisions based on the occurrence of one or more specific events in particular relationship to each other. An example of the use of displays to monitor events are the flight display systems used by aircraft pilots to operate and/or maneuver aircrafts during (1) take-off; (2) flight and (3) landing. One of the key instruments used by aircraft pilots is a display commonly referred to as a Primary Flight Display or PFD. The PFD provides graphical information regarding the status of the aircraft in flight. The PFD provides relatively little information when the aircraft is on the ground stationary or taxiing away from the landing strip after it has landed or taxiing toward the landing strip prior to take-off. When the aircraft is in flight, the PFD provides various information about the aircraft such as its roll (angle of wings relative to horizontal), heading, and the degree to which the nose of the aircraft is pointing upwards, downwards relative to the horizontal (commonly called “pitch”). The graphics depicted by the PFD are arranged in a standard format to allow a pilot to quickly locate a particular information by focusing in on the particular part of the display screen to which the information has been assigned.
Referring to
FIG. 1
there is shown a standard graphic and textual information arrangement for a PFD. Note that textual information is included with other graphical information to allow the pilot of the aircraft to determine the status of various sensor readings being provided to the aircraft while in flight. The sensor readings are various types of information from different sources which are converted to graphical signals that can be shown on the PFD. The “inverted V” shown at generally the center of the display represents the aircraft. The aircraft is shown in reference to the horizontal. Referring now to
FIG. 2
there is shown an annotated version of the PFD shown in FIG.
1
. Some of the information labeled in
FIG. 2
are used by the pilot while the aircraft is in flight, taking off or landing. For example, the “Zero Roll Reference” is used as a reference point for determining how much “roll” the aircraft is experiencing during flight. The roll bug depicts how much the aircraft is deviating from a zero roll orientation. The roll is a measure of how much the aircraft is rotated about its longitudinal axis (i.e., the axis that is oriented lengthwise of the aircraft). Also, various speeds are provided to the aircraft which are used by the pilot during take-off. Some of the critical speeds are referred to as “V-speeds.” V-speed V
1
represents the maximum speed during take-off at which the pilot must take the first action (e.g., apply brakes, reduce thrust, deploy speed brakes) to stop the airplane. V
1
also means the minimum speed in the takeoff, following a failure of an engine, at which the pilot can continue the take-off and achieve the required height above the takeoff surface within the takeoff distance. V
R
represents the speed at which the pilot must act to cause the airplane to rotate or pitch upwards during takeoff. A glossary of the various terms used to describe the displayed information in
FIG. 2
can be found in 14 CFR (Code of Federal Regulations) part
1
, of Federal Aviation Regulations Handbook which is incorporated herein by reference.
A perusal of the various labels in
FIG. 2
indicates that most, if not all, of the information being displayed by the PFD are applicable when the aircraft is in flight. Some of the information such as V
R
, V
1
and V
REF
are extremely critical in the control of the aircraft during take-offs and landings. V
REF
is a critical speed used during approaches and landings. The aircraft's specific location on the runway prior to and during take-off is important to know for the proper operation of the aircraft. For example, for take-offs, the aircraft should be traveling at a certain speed at a certain point on the runway for a proper and safe take-off. The specific point on the runway at which the aircraft is to have a certain speed, such as V
R
, is one type of information that is not provided by a standard PFD. Various other information that can be extremely useful to a pilot of an aircraft during takeoffs, landings and during flight either are not available to the pilot or are not provided by the PFD. These types of information can be easily displayed on the PFD, but at the risk of (1) adversely affecting the clarity of the standard information that is typically displayed on the PFD and (2) modifying the particular arrangement of the information to accommodate for the additional information being displayed. The clarity of the information being displayed is adversely affected because more information is being displayed in the same area and therefore an information clutter develops which makes it more difficult to read the display and distinguish between various pieces of information. The traditional arrangement of the information may have to be modified to a certain extent to allow for the additional information being displayed. A modification in the arrangement of the displayed information results in pilots having to be retrained so they can quickly locate certain types of information at certain critical times during landings, take-offs or even during flight. More generally, the additional information to be displayed visually affects the overall appearance of the display so that a defined standard display will not only lose its clarity of appearance but also lose the advantages gained in having such a standard design. What is therefore needed is a technique for displaying additional information on a display already depicting information arranged in a standard or well defined arrangement without adversely affecting the overall clarity of the standard arrangement and without modifying the standard arrangement.
SUMMARY OF THE INVENTION
The present invention provides a display generation system and method for generating at least one underlay image having an embedded safety pattern and causing such underlay image to be displayed simultaneously with an overlay image
Glaze Patrick Kemp
Jorgensen John Russell
Krohn Patrick Gerald
Naimer Hubert
Eisen Alexander
Greenberg & Traurig, LLP
Narcisse Claude R.
Universal Avionics Systems Corporation
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