SIGI This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "SIGI".
Space Integrated GPS/INS (SIGI) is a strapdown Inertial Navigation Unit (INU) developed and built by Honeywell International to control and stabilize spacecraft during missions. It has integrated global positioning/inertial navigation to provide three navigation solutions: Pure inertial, GPS-only and blended GPS/INS. SIGI have been employed on the International Space Station[1], the Japanese H-II Transfer Vehicle (HTV)[2] the Boeing X-37[3] and X-40.
SIGI is also proposed as the primary navigation system for the Orion (spacecraft), which is scheduled to replace the Space Shuttle.
Pitot-static instruments: Altimeter · Airspeed indicator · Machmeter · Variometer
Gyroscopic instruments: Attitude indicator · Heading indicator · Horizontal situation indicator · Turn and bank indicator · Turn coordinator · Turn indicator
Navigation: Horizontal situation indicator · Course Deviation Indicator · Inertial navigation system · GPS · SIGI ·
Other: Magnetic compass · Yaw string · Glass cockpit · EFIS