Global Positioning Systems, Inertial Navigation, and Integration

Chapter 9.3: INERTIAL SYSTEMS TECHNOLOGIES: INERTIAL SENSOR MODELS

9.3 INERTIAL SENSOR MODELS

Mathematical models for how inertial sensors perform are used throughout the INS development cycle. They include the following:

  1. Models used in designing the sensors to meet specified performance metrics.
  2. Models used to calibrate and compensate for fixed errors, such as scale factor and bias variations. The extreme performance requirements for inertial sensors cannot be met within manufacturing tolerances. Fortunately, the last few orders of magnitude improvement in performance can be achieved through calibration. These models are generally of two types:
    (a) Models based on engineering data and the principles of physics, such as the models carried over from the design trade offs. These models generally have a known cause for each observed effect.
    (b) Abstract, general-purpose mathematical models such as polynomials, used to fit observed error data in such a way that the sensor output errors can be effectively corrected.
  3. Error models used in GNSS/INS integration for determining the optimal weighting (Kalman gain) in combining GNSS and INS navigation data.
  4. Sensor models used in GNSS/INSS integration for recalibrating the INS continuously while GNSS data are available. This approach allows the INS to operate more accurately during periods of GNSS signal outage.

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