WO2003031915A1 - Precision perspective flight guidance symbology system - Google Patents
Precision perspective flight guidance symbology system Download PDFInfo
- Publication number
- WO2003031915A1 WO2003031915A1 PCT/US2002/025635 US0225635W WO03031915A1 WO 2003031915 A1 WO2003031915 A1 WO 2003031915A1 US 0225635 W US0225635 W US 0225635W WO 03031915 A1 WO03031915 A1 WO 03031915A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- qfpv
- pilot
- aircraft
- symbol
- symbology
- Prior art date
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
- G01C23/005—Flight directors
Definitions
- the invention relates generally to aircraft guidance systems, and more particularly to a guidance display that uses a predictive flight path, or performance, symbology set.
- a pilot In order to reduce tracking errors and pilot workload, a pilot must be provided with increased situational awareness of an aircraft the pilot is flying with respect to a desired flight path. Additionally the pilot must be aware of the actual aircraft performance, or flight path vector (FPV), the desired, or commanded, aircraft performance, and the predicted aircraft performance.
- FV flight path vector
- the use of a perspective display with a predictive flight path, or performance, symbology set provides increased situational awareness.
- Perspective displays with predictive symbology permit a pilot to "see" what will be required, or demanded, of the aircraft to maintain a desired flight path, as well as where the aircraft will be in a finite period of time. With the increased situational awareness, the pilot's workload is lower, thereby permitting better flight management.
- Flight director guidance for critical maneuvers is essential for precision navigation requirements.
- Known guidance symbology such as Delta- Veebar and Two-Bar, work well, but are limited in their ability to display future flight path information to the pilot and/or the results of pilot control input. Both Delta-Veebar and Two-Bar guidance symbology are based on compensatory tracking tasks.
- Compensatory tracking tasks are derived by monitoring actual aircraft attitude against commanded attitude during flight, and actual cross-track error against commanded cross-track during flight.
- Guidance errors are generally computed as the difference between guidance commands and sensed aircraft state. The errors are sent to flight director algorithms, which generate steering commands. These commands appear as flight director symbology on a cockpit display and direct the pilot where to position the lateral stick (roll), thrust control lever (power), and the longitudinal stick (pitch). If the pilot responds with the appropriate control inputs to satisfy the flight director steering commands, the aircraft will converge on the reference values selected.
- Symbology based on compensatory tracking tasks are designed to provide a pilot with command guidance instructing a pilot to make flight adjustments to guide an aircraft from an off-course situation to return to a nominal, or null error, solution.
- Compensatory tracking does not provide the pilot with information indicating how far off course the plane is, nor what flight control input is required to regain course centerline. Therefore, the pilot must constantly monitor command and the results of control inputs.
- compensatory tracking does not provide flight path predictability, and displays that utilize compensatory symbology require much cognitive processing by the pilot and cause heavy pilot mental workload leading to errors, especially in high workload constrained terminal areas, or during low altitude operations.
- perspective display sets or three-dimensional (3D) displays
- 3D tunnels consisting of a series of rectangles connected by lines through the corners.
- a predictive flight path symbology system for increasing pilot situational awareness of an aircraft.
- the system includes a pilot display, and a precision pathway flight guidance (PPFG) symbology set displayed on the pilot display.
- the PPFG symbology set includes broken line symbols representing an open guidance tunnel and providing flow field data, a half-bracket symbol to indicate that the aircraft is no longer in the open tunnel represented by the broken line symbols and the direction to turn to re-intercept the guidance tunnel, and a quickened flight path vector (QFPV) symbol to provide the pilot with predictive flight path information.
- QFPV quickened flight path vector
- a method for increasing pilot situational awareness of an aircraft utilizing a predictive flight path symbology set.
- the method includes utilizing an open tunnel bounded by broken lines symbol to provide flow field data, utilizing a half-bracket symbol to indicate that the aircraft is no longer in a tunnel, and utilizing a quickened flight path vector (QFPV) symbol to provide the pilot with predictive flight path information.
- QFPV quickened flight path vector
- a precision pathway flight guidance (PPFG) symbology set for increasing pilot situational awareness of an aircraft.
- the PPFG symbology set includes broken line symbols representing an open tunnel and providing flow field data, a half- bracket symbol to indicate that the aircraft is no longer in the open tunnel represented by the broken line symbols, and a quickened flight path vector (QFPV) symbol to provide the pilot with predictive flight path information.
- QFPV quickened flight path vector
- the PPFG symbology set further includes a quickened command reference frame configured to indicate a commanded location in which the pilot is to locate the QFPV in order to satisfy on-course tracking requirements, a longitudinal pitch trim symbol configured to maintain a desired pitch of the aircraft by the pilot adjusting the trim of the aircraft to align the longitudinal pitch trim symbol with the QFPV, and a power trim symbol configured to maintain a desired trim of the aircraft by the pilot adjusting power of the aircraft in order to position the power trim symbol level the QFPV.
- a quickened command reference frame configured to indicate a commanded location in which the pilot is to locate the QFPV in order to satisfy on-course tracking requirements
- a longitudinal pitch trim symbol configured to maintain a desired pitch of the aircraft by the pilot adjusting the trim of the aircraft to align the longitudinal pitch trim symbol with the QFPV
- a power trim symbol configured to maintain a desired trim of the aircraft by the pilot adjusting power of the aircraft in order to position the power trim symbol level the QFPV.
- Figure 1 is a graphical representation of a predictive flight path symbology system including a flight path vector based precision pathway flight guidance (PPFG) symbology set, used in accordance with one embodiment of the present invention
- PPFG precision pathway flight guidance
- Figure 2 shows a half bracket symbol included in the
- Figure 3 is a graphical representation of the predictive flight path symbology system shown in Figure 1 utilized with a 3D database.
- System 10 includes a FPV based precision pathway flight guidance (PPFG) symbology set 12 and a pilot display 14, on which PPFG symbology set 12 is displayed.
- PPFG precision pathway flight guidance
- PPFG symbology set 12 includes an open tunnel bounded by broken tunnel lines 16 that provides flow field data, such as a Boeing Philadelphia broken line open tunnel, a 'quickened flight path vector (QFPV) symbol 18 that indicates predictive aircraft state, such as a Delft QFPV, and a 'quickened' command reference frame 22 symbol into which a pilot is to place QFPV 18, such as a Kunststoff command reference frame.
- QFPV flight path vector
- PPFG symbology set 12 includes a pitch trim cue, or symbol, 26, such as a NASA Ames longitudinal trim command cue, that is utilized by the pilot to maintain a desired aircraft pitch, and a power trim cue, or symbol, 30, such as an Ames power cue, that is utilized by the pilot to maintain a desired trim on the aircraft.
- a pitch trim cue, or symbol, 26 such as a NASA Ames longitudinal trim command cue, that is utilized by the pilot to maintain a desired aircraft pitch
- a power trim cue, or symbol, 30, such as an Ames power cue
- PPFG symbology set 12 provides pilots of rotorcraft/tiltrotor, or any suitable airborne platform, with an intuitive symbology set.
- PPFG symbology set 12 Using a high resolution two dimensional (2D) database (not shown), or three dimensional (3D) database (not shown), PPFG symbology set 12 combines precision waypoint geolocation with "quickened" predictive flight-path- vector and "tunnel-in-the-sky" pathway guidance.
- a 2D database displays PPFG symbology set 12 either overlaying a map type display or accompanied by a map type display, as shown in Figure 1.
- a 3D database displays PPFG symbology set 12 either overlaying a synthetic vision type display or accompanied by a synthetic vision type display, as shown in Figure 3 described below.
- Waypoint geolocation can be determined by any suitable positioning system, such as a global positioning system (GPS).
- GPS global positioning system
- PPFG symbology set 12 provides an instrument approach guidance symbology system that enables pilots to execute steep (>4° glide slope) and normal ( ⁇ 4° glide slope) precision instrument approaches during instrument meteorological conditions (IMC) flight and/or instrument flight rules
- PPFG symbology set 12 enables a pilot to execute normal IMC flight, IFR flight, and low-altitude terrain flight/terrain avoidance (TF/TA), in near zero visibility.
- TF/TA symbology is driven by altitude data derived from a terrain digital map and DFAD/DFTED terrain elevation data.
- Aircraft position is provided by an INS/GPS update of actual aircraft position, which is updated and validated against an actual digital map position and an INS predicted position.
- Terrain elevation data from the terrain digital map, and aircraft altitude from an air data system and a radar altimeter, is provided to aircraft flight data computers.
- the elevation data and aircraft altitude are then compared against predicted, or required, aircraft actual altitude and a selected, or commanded, low altitude clearance altitude. Errors from commanded and actual, or predicted, elevation and aircraft position are provided to the pilot as the base of the tunnel pathway to be flown.
- PPFG symbology set 12 When employed on an aircraft guidance display, PPFG symbology set 12 presents a fully anticipatory perspective display, wherein the pilot has a pictorial display of the path to follow. PPFG symbology set 12 provides a tunnel type guidance systems, which requires reduced pilot cognitive process because a pilot merely needs to "stay between the lines.” The upper boundary of the open tunnel, formed by tunnel lines 16, acts as a power cue to indicate above glide slope conditions. An above glide slope condition indicates a requirement for increased descent gradients and power reduction and/or increase in rate of decent. PPFG symbology set 12 is anticipatory, such that it shows the pilot exactly where he is, and needs to be, thereby providing the pilot with an immediate indication of aircraft reaction to any control input, and immediately whether the control input satisfied a required demand.
- QFPV 18 is quickened, such that QFPV 18 is temporally placed at a finite distance or period of time ahead of the aircraft. Thus, QFPV 18 points where the aircraft will be at that fixed future moment in time. This permits the pilot to anticipate the direction and amount of control input required to fly a required path, or track, as well as the predicted result of that input.
- the open tunnel bounded by broken lines 16 displays a predetermined amount of the tunnel, or pathway, thereby reducing display clutter. For example, only sixty seconds of the tunnel are displayed.
- Broken lines 16 provide flow field data by banking, climbing, descending, and turning as the pathway turns and descends or climbs.
- the tunnel, or pathway provides anticipatory flight control input cues to the pilot.
- pilots keep QFPV 18 within quickened command frame 22, which is displayed temporally in front of the aircraft, for example 4.5 seconds.
- Tunnel height and width follow a 4/5 ths format that is linear as a function of airspeed. For example, tunnel height and width will vary from a maximum of 400 x 500 feet at air speeds above 250 KCAS to a minimum of 100 x 125 feet at air speeds less than, or equal to, 50 KCAS.
- Quickened command frame 22 is 'quickened' to be a predetermined fixed distance, or period time, ahead of the aircraft path. Additionally, quickened command frame 22 remains displayed at the fixed distance, or period of time, in front of the aircraft regardless of air speed. Quickened command frame 22 is used to indicate a 'command location' in which the pilot places QFPV 18 to satisfy tracking requirements. QFPV 18 is designed to be coplanar and cotemporal with quickened command frame 22.
- Pitch trim cue 26 is used to indicate the proper longitudinal pitch needed to maintain QFPV 18 within quickened command frame 22.
- pitch trim cue is an orange delta displayed adjacent a right wing of QFPV 18.
- the pilot maintains a desired pitch of the aircraft by maneuvering the aircraft so that the right wing of QFPV 18 remains aligned with pitch trim cue 26.
- Power command cue 30 is used to indicate power requirements needed to maintain QFPV 18 within quickened command frame 22.
- the power command cue 30 is a yellow delta adjacent a left wing of QFPV 18.
- the pilot maintains a desired power trim of the aircraft by maneuvering the aircraft so that the left wing of QFPV 18 remains level with power trim cue 30.
- Figure 2 shows a half bracket symbol 34 included in PPFG symbology set 12 (shown in Figure 1).
- Figure 2 shows half bracket 34 in two configurations. In a first configuration, half bracket 34 is shown having legs extending in a first direction, for example right or down. In the second configuration, half bracket 34 is shown having legs extended in a second direction opposite the direction shown in the first configuration, for example left or up.
- Half bracket 34 indicates when the pilot is 'out of the tunnel'.
- Half bracket 34 is designed to be directional such that half bracket 34 indicates whether the tunnel is above, below, left, or right. By knowing were the tunnel is with respect to the aircraft the pilot can redirect the aircraft so that QFPV 18 (shown in Figure 1) re-intercepts the tunnel.
- half bracket 34 When a pilot utilizes half bracket 34 to guide the aircraft on a flight path that will cause QFPV 18 to re-intercept the tunnel, as the aircraft reaches a reciprocal heading, i.e. 180° of turn away from the tunnel, half bracket 34 will convert from the first configuration to the second configuration, thereby indicating that the pilot is now turning toward the tunnel. For example, when the pilot utilizes half bracket 34 having the first configuration, when the aircraft reaches a reciprocal heading half bracket 34 will convert to the second configuration.
- Figure 3 is a graphical representation of predictive flight path symbology system 100, including flight path vector based PPFG symbology set 12 (shown in Figure 1) utilized with a 3D database (not shown).
- Components in Figure 3 identical to components in Figure 1 are identified in Figure 3 using the same reference numerals as used in Figure 1. While the two dimensional (2D) database illustrated in Figure 1 displays data in two dimensions, for example height and width, the three dimensional (3D) database illustrated in Figure 3 displays data in three dimensions, for example height, width, and depth, thereby depicting objects with perspective.
- PPFG symbology set 12 When PPFG symbology set 12 is utilized with a 3D database, PPFG symbology set 12 is displayed either overlaying a synthetic vision type display or accompanied by a synthetic vision type display. Overlaying PPFG symbology set 12 on a synthetic vision display allows the pilot to not only see the course to flown, but the relationship of the underlying terrain. Therefore, little visual and mental interpretation by the pilot is required.
- the symbology set of the present invention is especially suited for use in aircraft having steep approach angles, or aircraft required to descend and decelerate to a hover, or near hover, the symbology set is not limited to such applications and is applicable for use in any aircraft. Effectively designed and implemented, PPFG symbology is capable of replacing traditional, workload intensive, Two-Bar and Delta-Veebar flight director terminal approach guidance while providing smaller flight technical error and reduced pilot workload.
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL16052102A IL160521A0 (en) | 2001-10-11 | 2002-08-12 | Precision perspective fight guidance symbology system |
EP02757085A EP1434972B1 (en) | 2001-10-11 | 2002-08-12 | Precision perspective flight guidance symbology system |
IL160521A IL160521A (en) | 2001-10-11 | 2004-02-23 | Precision perspective flight guidance symbology system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/975,624 | 2001-10-11 | ||
US09/975,624 US6798423B2 (en) | 2001-10-11 | 2001-10-11 | Precision perspective flight guidance symbology system |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2003031915A1 true WO2003031915A1 (en) | 2003-04-17 |
Family
ID=25523216
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2002/025635 WO2003031915A1 (en) | 2001-10-11 | 2002-08-12 | Precision perspective flight guidance symbology system |
Country Status (4)
Country | Link |
---|---|
US (1) | US6798423B2 (en) |
EP (1) | EP1434972B1 (en) |
IL (2) | IL160521A0 (en) |
WO (1) | WO2003031915A1 (en) |
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- 2002-08-12 IL IL16052102A patent/IL160521A0/en unknown
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Also Published As
Publication number | Publication date |
---|---|
US20030071828A1 (en) | 2003-04-17 |
EP1434972B1 (en) | 2012-05-30 |
EP1434972A1 (en) | 2004-07-07 |
IL160521A (en) | 2014-06-30 |
US6798423B2 (en) | 2004-09-28 |
IL160521A0 (en) | 2004-07-25 |
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