How do you calculate cruising altitude?

How do you calculate cruising altitude?

You must know your current altitude: TOD (top of descent) is 3 x your current altitude – destination airport altitude / 1,000 (example: a cruise altitude 32,000 ft. x 3 = 96,000 – 1,500 (destination airport altitude) = 94,500 / 1,000 = 94.5 miles away you begin your descent.)

How do you calculate field pressure altitude?

Find pressure altitude

  1. Subtract the current altimeter setting from the standard pressure of 29.92.
  2. Multiply by 1,000.
  3. If you have a negative number, subtract it from the field elevation. Add a positive number.

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How can you calculate the altitude of an aircraft?

You can’t directly calculate the altitude of an aircraft from any set of control settings. The altitude is dependent on the history of the aircraft. For example: Fly level at full power for one minute, and pitch up suddenly. You will be near the ground, having quite some speed. Climb at full power for a minute.

What are the variables in a flight simulation?

For the purposes of very simple simulation, and assuming aircraft is on ground at certain airport at certain altitude. The starting variables are then nothing but a throttle position, which over time increases, which translates into speed. And once the aircraft is airborne also the pitch.

How can trigonometry be used to calculate altitude?

If you know the airspeed of the aircraft in feet per second, you should be able to use trigonometry to calculate of that speed how much is horizonatal and how much vertical. The vertical component can then be used to adjust the altitude and the horizontal the position over the ground.

How is the altitude from sea level read?

I guess altitude from sea level in the real aircraft is read from barometer, while for the altitude from ground a radar is used. For the purposes of very simple simulation, and assuming aircraft is on ground at certain airport at certain altitude.