Integrated navigation and guidance systems

Bibliographic Information

Integrated navigation and guidance systems

Daniel J. Biezad

(AIAA education series)

American Institute of Aeronautics and Astronautics, c1999

Available at  / 10 libraries

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Description and Table of Contents

Description

Beginning with the basic principles of navigation, this work takes a step beyond introductions with a concise look at the flight applications of inertial navigation systems integrated with Global Positioning System (GPS) satellite systems. Written at the senior engineering college level, the textbook takes a tutorial approach, weaving interrelated disciplines together with interactive computer exercises and AINSBOOK software for error analysis and Kalman filter simulation. Readers should benefit from engineering, teaching and flying experience of Professor Biezard. The AINSBOOK software is the work of Dr Stanley F. Schmidt, a scientist with experience at NASA and in the aerospace industry. This guide offers a technical jump start with a look at traditional navigation radio aids, inertial guidance systems and Kalman filters, and launch into GPS applications to navigation, precision approach and landing, attitude control and air traffic control. Figures, photos and tables add to the textbook's accessibility, making it a reader-friendly reference for any aerospace professional working in development and testing of advanced integrated navigation systems.

Table of Contents

  • Principles of Navigation and the Concept of an Integrated Navigation System
  • Newton's Laws Applied to Navigation (Geodesics, Basic Reference Frames, Simplified Aerospace Vehicle Equation)
  • Inertial Navigation Systems (INS) and Global Positioning System (GPS)
  • Uncertainty in Navigation, INS Error Propagation, Probabilities, Autocorrelation and the Method of Least Squares
  • Kalman Filters and Their Key Role in the Integration of Aircraft Avionics Systems
  • GPS Theory and its Application to Navigation (Including System Accuracy)
  • GPS Application to Precision Approach and Landing, Attitude Control and Air Traffic Control
  • Flight Testing of Navigation Systems
  • Computer Exercises.

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