Global Positioning Systems, Inertial Navigation, and Integration

Chapter 9.3.5: INERTIAL SYSTEMS TECHNOLOGIES: Auxilliary Sensors

9.3.5 Auxilliary Sensors

9.3.5.1 Attitude Sensors Nongyroscopic attitude sensors can also be used as aids in inertial navigation. These include the following:

Magnetic sensors are used primarily for coarse heading initialization, to speed up INS alignment.

Star trackers are used primarily for space-based or near-space applications. The U-2 spy plane, for example, used an inertial-platform-mounted star tracker to maintain INS alignment on long flights.

Optical alignment systems used on some space launch systems. Some use Porro prisms mounted on the inertial platform to maintain optical line-of-sight reference through ground-based theodolites to reference directions at the launch complex.

GNSS receiver systems using antenna arrays and carrier phase interferometry have been used for heading initialization in artillery fire control systems, for example, but the same technology could be used for INS aiding. The systems generally have baselines in the order of several meters, which could limit their utility for some host vehicles.

9.3.5.2 Altitude Sensors These include barometric altimeters and radar altimeters. Without GNSS inputs, some sort of altitude sensor is required to stabilize INS vertical channel errors.

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