Hardware software of integrated insert-satellite navigation system for unmanned aerial vehicles PP184
The integrated inertia - satellite navigation system (ISN) is designed to determine navigation parameters of the moving object. The core of ISN is platform - free inertial navigation system (Sins) built on microelectromechanical accelerometers and angular velocity sensors. Bins Integrana (Retail on platinum alone) satellite navigation magnetometer and barometric altimeter. Allows: predict the admissibility of optimal signals NS configurations of GPS and GLONASS systems; evaluate accuracy factor of accuracy of navigation definitions; wire outlet coordinates and consumer time by GPS and GLONASS signal
INTELLECTUAL PROPERTY STATUS
4 patents and 2 copyright certificates Of Ukraine were obtained.
The developed EISC can be installed on unmanned aerial vehicles of various types production of Ukraine and other countries.
MAIN CHARACTERISTICS OF THE DEVELOPMENTThe developed ETSS is able to determine: angular speed with an accuracy of 0. 16 ° / s; acceleration of the object 1. 5 mg; height with an accuracy of 3 m; angles - a roll and a pitch with an accuracy of 1°, a course with an accuracy of 2°, speed up to 0. 1 m / s. The coordinates of the plane The ETSS determines with an accuracy of 5 m. ETSS enables: determining the angular velocity of an object in the range ± 450 ° / s; definition of acceleration of the object in the range of ± 18, ± 10 g; definition of flight altitude in the range from 0 to 3500 m; definition of airplane angles - a roll in the range of ± 180°, pitch ± 90°, course from 0° to 360°; definition of the speed of unmanned aircraft in the range from 0 to 400 m / s. These figures are consistent with the ETSI known firm SGS (France).
THE DEVELOPMENT READINESS STATUS
There were created a prototype and software. The expected characteristics were confirmed.