OBC provide the implementation of wide range of tasks of spacecraft and launch vehicles Control Systems.
Term “versatile” means the possibility of versatile navigation complex application in Control Systems of various aerospace vehicles: launch vehicles, small rockets, Unmanned Aerial Vehicles of medium and heavy class, cargo-and-passenger aircrafts. Versatile Navigation Complex functioning is based on integrated inertial-satellite navigation system concepts.
Inertial measurement unit and navigation computer are developed in common form factor. Versatile navigation complex integration with other external systems (radio altimeter, barometric altimeter, air signals system, odometers etc.) is determined by tasks to perform by concrete vehicles. Tact of data pickup:
Navigation task integrated with GPS user equipment is computed with tact 5 ms.
This device is intended for spacecraft Control Systems application. Device functioning is based on strap-down stellar inertial navigation system concept.
FOG data processing is performed in special computer with tact 5 ms, stellar measurement system measurements are used for inertial data specification with tact 200 ms.
Our services run deep and are backed by over ten years of experience.