Descent

A Descent performance model is comprised of two or more points that define the characteristics of the performance model. These points are displayed in a chart at the top of the display and defined in a table below. The Descent performance model allows you to define descent profile by time, distance, and fuel to climb to a given altitude, similar to how aircraft operating manuals are configured. This performance model is determined by the data entered without regard to aerodynamics, propulsion characteristics, or weight. Descent can be considered an altitude varying version of Basic Descent. Use this model if you know specific elements of an aircraft descent profile. To access the descent model,

  1. Open aircraft properties.
  2. Right click on "Descent.”
  3. Select new model type. This Descent model is “AGI Descent Model”.

Chart and Table

You can add new points by left-clicking in the profile to add a point at that specific location. You can also add a new point before the currently selected point by clicking Insert Item and defining the point in the window that appears. You can edit existing points by double-clicking any of their fields in the table or by clicking Edit Item ... to edit the currently selected point in a separate window; in addition, you can edit the altitude of a point by double-clicking it in the chart.

Click Remove Item to remove the currently selected point. A point that is displayed in red is an invalid entry - one which is not a monotonic increase of fuel consumption, time elapsed, and downrange distance over the previous entry. Click Remove Invalid Items to remove all points that are currently indicated as being invalid.

The fields that define each point in the model are described in the following table.

Field Description
Altitude The aircraft's altitude in feet. You cannot specify an altitude below sea level (0). If a procedure is specified that requires the aircraft to fly below sea level, the performance models in effect at sea level will be applied to that procedure.
Downrange The ground distance in nautical miles from the first point in the model to the aircraft's position at this point.
Elapsed Time The amount of time that has elapsed since the first point of the model.
Segment Time The amount of time that has elapsed since the previous point of the model.
Airspeed (TAS True Airspeed: the speed that the aircraft is moving relative to the airmass that it is flying in., CAS Calibrated Airspeed: the speed reported by the airspeed indicator, corrected for position and instrument error., EAS Equivalent Airspeed: the airspeed at sea level (International Standard Atmosphere) at which the dynamic pressure is equal to the dynamic pressure at the aircraft's current true airspeed and altitude., Mach The ratio of the aircraft's speed and the speed of sound at the aircraft's altitude, with local atmospheric conditions.) Displays the calculated airspeed during this segment of the model.
Fuel The amount of fuel required to climb from or descend to sea level for the associated altitude; this number must be a monotonic increase or decrease, respectively, from the previous entry.
Fuel Flow The amount of fuel used in pounds per hour.

Chart Commands

You can also interact with the chart using a right-click menu available within the actual chart display; this menu is defined in the table below.

Table - Right-Click CommandsClosed

Command Description
Insert Mode Enables a left-click in the chart to add a new point at the cursor's location.
Select Mode Enables a left-click in the chart to select the point in the table that corresponds to the selected point.
Zoom Mode Transforms the cursor within the chart to a magnifying glass and allows you to left-click and drag over an area of the chart to zoom in upon. Using the scroll-bars, you can move around the chart while zoomed.
Undo Zoom Zooms out the chart display to its default view.
Profile Data Opens the Profile Data window for the selected point. The Profile Data window displays mission data at the point in the performance model profile at which it is invoked from the right-click command menu. Click Copy to Clipboard to copy the data in this window to the clipboard.
2nd Y Axis... Allows you to define the secondary Y axes of the chart.
Airspeed Display Allows you to set the airspeed reference of the performance model - true airspeed (TAS), calibrated airspeed (CAS), equivalent airspeed (EAS), or Mach number.
Font Size Provides a sub-menu that allows you to select the font size of profile labels - small, medium, or large.
Grid Options Provides a sub-menu that allows you to define the display of grid lines within the profile.
Mark Data Points Displays individual data points along the profile line.

Other Options

There are several other options available outside of the chart and table.

Table - Other OptionsClosed

Field Description
Airspeed Display Allows you to set the airspeed reference of the performance model - true airspeed (TAS), calibrated airspeed (CAS), equivalent airspeed (EAS), or Mach number.
Use Aero/Propulsion Fuel Flow Select this check box to use the fuel flow calculated by the aerodynamics and propulsion strategies defined in the active acceleration performance model; if the acceleration performance model is not set to calculate fuel flow, then fuel flow will not be calculated for this performance model, either.
Scale Fuel Flow by Non Std Density Select this check box to scale the fuel flow based on the aircraft's actual altitude. If this option is disabled, the fuel flow will be calculated at the Default Cruise Altitude (if available), or at sea level.
Initial Level Off for Acceleration If enabled, the aircraft will level off and accelerate or decelerate until its airspeed is within the defined Relative airspeed tolerance, and only then begin its climb or descent. This models the common pilot practice of achieving the aircraft's optimal climb or descent airspeed at level flight before beginning a climb or descent.