Direct conrol system of air means

DCS is intended to generate command control signals to the aircraft (helicopter) to keep the aircraft on a given flight path and altitude during the flight by the route, arrival actions for landing on a given special area in standalone mode.

When combined with the Early Warning System to be closer to the earth  -  Implementation of the optimal flight path traversal (rounding) of obstacles or areas of dangerous weather conditions.

1. Aerobatic display control:

2. Module GNSS (GPS) and the antenna:

Aircraft Control Modes:

• Manual, director, automatic;

Modes of Operation 

• “Route”, “return”, “landing”, “re-entry”, “relief”;

The calculation of the flight with route or track approach:

• Automatic and continuous indication of the location of aircraft in the polar and geographical coordinates;
• An indication of the line specified paths (flight path) of the aircraft to exit it at the optimal trajectory;
• Signaling when aircraft comes through the given checkpoint;
• Operational data typing a new specified route point again when the flight path was changed (bypassing the severe weather, etc.);
• Ensure aircraft input in the starting point to come near to a given trajectory (initial stage);
• Signaling  when the aircraft comes near to the minimum safe altitude of the stages of the route;
• Calculation of wind direction and speed (automatic or on request);
• Display the current estimated navigation data taking into account the drift angle;
• An autonomous the definition of bearing on a given airport (platform);
• An autonomous definition of altitude, route speed and track angle with the magnetic board systems failures during the flight on the route;
• Forecast the trajectories of aircraft and some of the navigation parameters in the absence of signals of GNSS.

Construction of the landing maneuvers:

• Landing (second landing) on the selected path;
• Calculation of the trajectory of landing at the lower rate of precipitation;
• Display of the landing maneuver location of aircraft;
• Select the type of glide path taking into account maneuvering of aircraft;
• Set and alarm the minimum safe altitude at the aerodrome;
• Displays current estimated navigation data of the given line rate, the glide path and the current distance to touchdown;
• An autonomous definition of altitude, ground speed and track angle with the magnetic board systems failures during landing;
• The distance forecast to touchdown in the absence of signals of GNSS;
• Detection of early landing and a warning about the crew in accordance with the requirements. 

Combination with an early warning system to be closer to the earth:

• Form the direct control command when crawling (rounding) of the terrain on the most favorable trajectory;
• Prevent collisions with obstacles - the calculation of the optimal trajectory traversal (rounding) of obstacles when alarm was triggered such "Ahead of the earth» («Terrain Ahead») or "In front of an obstacle» («Obstacle Ahead»);
• Alarm on roll values limit  “Roll is large”;
• Jeppesen database information.
  

Small-sized color LCD display: