MIT ICAT Inertial Reference Unit Integrate acceleration from known position and velocity ∨e|ocit 口 Position Need Heading 口Gyos Mechanica Lasel · Can get Attitude Q Artificial Horizon(PFD. HUD) Drift Errors d IRU unusable in vertical direction(need baro alt) 日 Inflight Correction DME GPS Star Sighting for Space Vehicles Measurement Give Attitude also 777 Analytical RedundancyMIT ICAT Inertial Reference Unit y Integrate acceleration from known position and velocity Velocity Position y Need Heading Gyros Mechanical Laser y Can get Attitude Artificial Horizon (PFD. HUD) y Drift Errors IRU unusable in vertical direction (need baro alt) Inflight Correction DME GPS Star Sighting for Space Vehicles y Measurement Give Attitude Also y 777 Analytical Redundancy