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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 DEVELOPMENT
THE DEVELOPMENT READINESS STATUS
There were created a prototype and software. The expected characteristics were confirmed.