Drone flight control

Reference navigation

The UAV Navigation Control System (FCS) can create a movable reference flight plan. This function allows the execution of automatic ISTAR or related maritime operations for moving targets.

GNSS refused to navigate.

Excellent performance GNSS environment rejection and interference threat High-quality components and designed EMI compatible EMC testing MIL-STD-461) Advanced estimation methods can reduce the impact of labor intensity. When reliable GNSS signals become unavailable, it can accurately navigate.

Safety features

Many emergency measures to prevent sensor failure. Multi-path planning can specify the screen area of the path selection, the expected input and output channel capabilities. FTS... In addition, the transformer has buoyancy protection, which can effectively detect engine failure and start. Automatically add distance and free safe landing

Simple task planning

The system can perform different high-level tasks and operate automatically at existing points. These operations make mission planning easier: monitor the actions of the infrastructure navy, track, reference, and actions may be fully automated, including ascent and descent. Use improved source code or GNSS solutions, namely, RTK, NSS, DGS, and

Multi-mission drone

UAV navigation solutions help can fly UAV at the same time. Three people can be in different configurations: one controller to control multiple drones or to operate multiple drones to control.

Certified hardware

Hardware MIL-STD-810F MIL-STD 461F This is proof that the system has passed independent tests, ensuring excellent performance under adverse conditions.

Since 2547, UAV navigation has provided a complete flight control solution configuration and total one-year size. Currently, global customers include general aircraft manufacturers, VTOL platforms, design, piloting and hybrid years. Manual platform, low-speed UAV, biplane UAV, medium and high altitude, MALEYH41, high altitude satellite, holmium HAPS 4141. Aircraft and other irregular wings The system can control wings of various sizes, from a small electric platform, two kilograms to drones. The largest wing is currently 250 kg in MTO1. The autopilot can safely control the interior of the aircraft. The flight bag and system are allowed to be loaded into the automatic conversion tank, and the conditions can be changed, such as if the drone discards the cargo, the weight of the aircraft changes during the flight

Development of UAV Navigation Hardware simulation program in the loop: HIL 41 Risks in the project development process, training in standards and emergency procedures. The virtual client platform is used to generate customized software to adapt to the flight characteristics of a specific aircraft. If necessary, customers with any special requirements can develop at this stage, for example, including other paid cameras. New features in the system

The autopilot is completely based on the flight safety platform, including a fully automatic recovery basis. Complex aviation planning, including health monitoring, configurable GPS, etc. In addition to the basics, the autopilot can also respond to loads. All kinds, including complex Jinba. (DST, UAV Vision, Octopus altimeter, altimeter, laser and other advanced functions. Geolocation and target tracking or high-precision and dynamic movement. Including runway movement, operation, holmium for maritime operations, and balloon take-off. UAV operation is not A precise single-track landing control solution for GPS systems using expensive RTK accounts

The solution includes air transportation planning and your action plan, including the creation of flight files and reference moves or intermediate points. Selection and emergency planning Autopilot adjusts the flight plan even when the plane takes off.

Although small, Thailand's UAV products have a complete autopilot system, which means that the unit includes all necessary sensors to fly. No need for additional sensors or housing to move the control surface. However, it can increase the system performance of external sensors, such as high-level sensors, fuel cells, etc.

Other special qualifications for the second year

Compact unit There is no need to use external sensors, inertial measurement unit, IMU 41 or task management computer are already integrated in one.

Online testing The OLHIC algorithm ensures the detection of the sensor's magnetic field strength and continuous international standards. Fly away This will help to accumulate errors in flight.