Composite normalized angle of attack indicating system
A composite normalized angle of attack indicating system provides a simultaneous display of both body angle of attack, such as in digital form, and normalized angle of attack for an aircraft. The display may be visually enhanced as stall is approached such as by zooming the body angle of attack digital display and/or by changing the color of the display. The normalized display also selectively displays an approach reference band when the flap setting is equal to or greater than 20 degrees.
1. A normalized angle of attack indicating system for use in an aircraft, the indicating system comprising a display gauge comprising:
fixed position markings to indicate a predetermined range of normalized aircraft angle of attack in a normalized display presentation, the predetermined range comprising a zero body angle of attack and a stall angle of attack with respect to the aircraft; and
a scale having a plurality of normalized scale segments associated with a plurality of flight phases within the predetermined range;
wherein the display gauge is configured to display an indicia of body angle of attack for the aircraft simultaneously with the normalized angle of attack for the aircraft for providing a composite simultaneous display of the body angle of attack along with the normalized angle of attack for the aircraft, the body angle of attack being dependent on constants for the aircraft.
2. The indicating system of claim 1 further comprising an approach reference band for the aircraft that is selectively displayed in the normalized display presentation when the fixed position markings correspond to a predetermined percentage of the stall angle of attack.
3. The indicating system of claim 1 wherein the body angle of attack indicia comprises a digital display of the body angle of attack.
4. The indicating system of claim 1 wherein the normalized angle of attack display presentation comprises a pointer indicia being movable along the scale between the fixed position markings in accordance with changes in the normalized angle of attack.
5. The indicating system of claim 1 wherein the plurality of normalized scale segments further comprise a scale segment based on the zero body angle of attack and a scale segment based on the stall angle of attack.
6. The indicating system of claim 1 wherein the body angle of attack display presentation is enhanced in response to a predetermined condition.
7. The indicating system of claim 6 wherein the predetermined condition comprises the body angle of attack value approaching the stall value for the aircraft.
8. The indicating system of claim 7 wherein the body angle of attack display presentation is further enhanced by dynamically zooming the body angle of attack display presentation in response to the predetermined condition.
9. The indicating system of claim 8 wherein the body angle of attack display presentation is further enhanced by changing coloration of the body angle of attack display presentation in response to the predetermined condition.
10. The indicating system of claim 1 wherein the scale of the normalized display presentation comprising the fixed position markings, is based on the equation
n
=
α
-
α
APP
α
SS
-
α
APP
*
-
90
where α represents the angle of attack
α App represents the approach reference angle of attack
and α ss represents the stick shaker angle of attack.
11. A display gauge for an aircraft, the display gauge comprising:
(a) a normalized angle of attack indicator comprising:
fixed position markings to indicate a predetermined range of normalized aircraft angle of attack in a normalized display presentation, the predetermined range comprising a zero body angle of attack and a stall angle of attack with respect to the aircraft; and
a scale having a plurality of normalized scale segments associated with a plurality of flight phases within the predetermined range; and
(b) a body angle of attack indicator that is configured to provide an indicia of a body angle of attack for the aircraft, the body angle of attack being dependent on constants for the aircraft;
wherein the normalized angle of attack indicator and the body angle of attack indicator are located adjacent to one another within the display gauge to provide a composite display that simultaneously indicates the body angle of attack alongside the normalized aircraft angle of attack of the aircraft.
12. The display gauge of claim 11 further comprising an approach reference band for the aircraft that is selectively displayed in the normalized display indicator when the fixed position markings correspond to a predetermined percentage of the stall angle of attack.
13. The display gauge of claim 11 wherein the body angle of attack indicia comprises a digital display of the body angle of attack.
14. The display gauge of claim 11 wherein the normalized angle of attack display indicator comprises a pointer indicia being movable along the scale between the fixed position markings in accordance with changes in the normalized angle of attack.
15. The display gauge of claim 11 wherein the plurality of normalized scale segments further comprise a scale segment based on the zero body angle of attack and a scale segment based on the stall angle of attack.
16. The display gauge of claim 11 wherein the body angle of attack display indicator is enhanced in response to a predetermined condition, and wherein the predetermined condition comprises the body angle of attack value approaching the stall value for the aircraft.
17. The display gauge of claim 16 wherein the body angle of attack display indicator is enhanced by dynamically zooming the body angle of attack display in response to the predetermined condition, or by changing coloration of the body angle of attack display in response to the predetermined condition.
18. The display gauge of claim 11 wherein the scale of the normalized angle of attack indicator comprising the fixed position markings is based on the equation
n
=
α
-
α
APP
α
SS
-
α
APP
*
-
90
where α represents the angle of attack
α App represents the approach reference angle of attack
and α ss represents the stick shaker angle of attack.
19. The display gauge of claim 11 wherein the display gauge is incorporated into an angle of attack indicating system for the aircraft and the angle of attack indicating system at least comprises:
one or more sensors configured to measure a raw angle of attack and one or more parameters associated with the aircraft;
at least one hardware processor coupled to the one or more sensors and configured to compute a stick shaker value and a flap position value;
at least one data concentrator unit coupled to the at least one hardware processor and configured to:
convert the raw angle of attack into a body angle of attack; and
convert the stick shaker value into a stick shaker body angle of attack based on a look up table.
20. A method for use by an angle of attack indicating system in an aircraft, the method comprising:
providing fixed position markings to indicate a predetermined range of normalized aircraft angle of attack in a normalized display presentation, the predetermined range comprising a zero body angle of attack and a stall angle of attack with respect to the aircraft; and
providing a scale having a plurality of normalized scale segments associated with a plurality of flight phases within the predetermined range;
wherein the display gauge is configured to display an indicia of body angle of attack for the aircraft simultaneously with the normalized angle of attack for the aircraft for providing a composite simultaneous display of the body angle of attack along with the normalized angle of attack for the aircraft, the body angle of attack being dependent on constants for the aircraft.