a) automatic flight design for photogrammetric flights;
b) possibility of determining the basic flight parameters of the mission: rate of climb, descent, progressive movement, hovering height at various stages of the mission;
c) possibility to program the flight route by points (flight altitude/ speed);
d) possibility to determine the take-off and landing points by selecting a place on the map using the touch screen/pointing device or by entering the geographical coordinates;
e) automatic landing at specified position in case of loss of steering signal/ power failure/ on operator’s command;
f ) switching off the engines at the end of the mission;
g) possibility to edit mission points during autonomous flight;
h) possibility to save and load; a previously prepared mission;
i) ability to visualise the course of the mission in 3D;
j) possibility to record and display flight parameters as a file with a frequency of up to 10 Hz.

k) after reaching the take-off point – switching to the automatic emergency landing mode in the PROMETHEUS capsule (trailer), after landing switching off the engines;
l) YAW axis control feature active during automatic return to the take-off point;
m) possibility to determine the front direction of the drone in relation to the position of the operator during the automatic return to the take-off point;
n) possibility of triggering an automatic landing at a predetermined location or during an event.