Dynamic detection of landing gear deployment

A system comprising:

• a processing device in communication with memory;
• and
• one or more tools in communication with the processing device, the tools to:
• dynamically generate a set of flight measurements, including the functional unit to dynamically obtain an altitude measurement, a distance to a destination measurement, and an airspeed measurement of an aerial vehicle;
• store the generated flight measurements in memory;
• compare each flight measurement to a respective threshold value to produce a landing scenario indication, wherein the comparison comprises the functional unit to:
• ascertain that the vehicle is within a defined above ground level based on the altitude measurement;
• ascertain that the vehicle is within a defined distance to a destination based on the distance to a destination measurement;
• and
• ascertain that the airspeed measurement is below a maximum gear extension speed;
• and
• convert the produced indicated into a landing gear protocol.

A computer program product comprising a computer-readable storage device having computer-readable program code embodied therewith, the program code executable by a processor to:

• dynamically generate a set of flight measurements, including the functional unit to dynamically obtain an altitude measurement, a distance to a destination measurement, and an airspeed measurement of an aerial vehicle;
• store the generated flight measurements in the memory;
• compare each flight measurement to a respective threshold value to produce a landing scenario indication, wherein the comparison comprises program code to:
• ascertain that the vehicle is within a defined above ground level based on the altitude measurement;
• ascertain that the vehicle is within a defined distance to a destination based on the distance to a destination measurement;
• and
• ascertain that the airspeed measurement is below a maximum gear extension speed;
• and
• convert the produced indicated into a landing gear protocol.