Landing assistance device and method for aircraft
A technology of aircraft and approach speed, applied in aircraft lander, position/direction control, vehicle position/route/altitude control, etc., can solve the problem of inability to predict and judge the driver
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[0039] In the situation schematically represented in FIG. 1 , an aircraft 1 wishes to land on a runway 2 during an approach landing phase, the usual length L of which is defined between a proximal threshold Sp and a distal threshold Sd. Aircraft 1 descends towards runway 2 at current approach speed V along current approach route 3 with current approach angle γ. When the aircraft 1 is at a horizontal distance X from the proximal threshold Sp, that is, vertically above the point 4 on the ground 5, the point 4 is at X distance from the proximal threshold Sp, and its current height on the current route 3 is equal to h.
[0040] In accordance with the landing maneuver rules associated with runway 2, in order to optimize the chances of a correct landing, the current approach path 3 of aircraft 1 must pass a reference point Po above the proximal threshold Sp with adjusted altitude ho and corresponding to the path 3 Start of straightening section 6. Also, follow these landing maneuve...
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