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 specific constants for the aircraft; and
wherein the body angle of attack display presentation is enhanced in response to a predetermined condition which comprises the body angle of attack value approaching the stall value for the aircraft, and 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.
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 further enhanced by changing coloration of the body angle of attack display presentation in response to the predetermined condition.
7. 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.
8. A normalized angle of attack indicating system for use in an aircraft comprising:
a plurality of sensors configured to measure a raw angle of attack and a set of parameters associated with the aircraft;
at least one hardware processor coupled to the plurality of 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,
convert the stick shaker value into a stick shaker body angle of attack based on a look up table, and
calculate an approach reference angle of attack based on the flap position value and the set of parameters associated with the aircraft; and
a display coupled to the at least one data concentrator unit and configured to:
display, based on at least the body angle of attack, the stick shaker body angle of attack and the approach reference angle of attack, a normalized angle of attack for the aircraft within a predetermined scale, wherein the predetermined scale comprises a plurality of normalized scale segments associated with a plurality of flight phases between a zero body angle of attack and a stall angle of attack,
display fixed position markings on the predetermined scale of normalized angle of attack in a normalized display presentation, and
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.
9. The indicating system of claim 8 wherein the display is further configured to selectively display an approach reference band for the aircraft in the normalized display presentation when the fixed position markings correspond to a predetermined percentage of the stall angle of attack.
10. The indicating system of claim 8 wherein the body angle of attack indicia comprises a digital display of the body angle of attack.
11. The indicating system of claim 8 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.
12. The indicating system of claim 8 wherein the plurality of normalized scale segments further comprise a scale segment based on the zero body angle and a scale segment based on the stall angle of attack for the aircraft.
13. The indicating system of claim 8 wherein the body angle of attack display presentation is enhanced in response to a predetermined condition.
14. The indicating system of claim 13 wherein the predetermined condition comprises the body angle of attack value approaching the stall value for said aircraft.
15. The indicating system of claim 14 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.
16. The indicating system of claim 15 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.
17. The indicating system of claim 8 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.
18. The indicating system of claim 8 wherein the look up table comprises the weight of the aircraft, the load factor and the center of gravity.
19. 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 specific constants for the aircraft; and
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.