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Navigation Guidance and Control

a
Course
Postgraduate
Semester
Electives
Subject Code
AE716

Syllabus

Principles of Inertial Navigation: Components, two-dimensional navigation – Coordinate systems – 3D strapdown navigation system – Strapdown system mechanizations – Attitude representation – Navigation equations expressed in component form – Effects of elliptic earth – Inertial Sensors: Gy- roscope principles, single-axis rate gyroscope, accelerometers, rate integrating gyroscope – Elements of guidance system – Guidance phases – Guidance trajectories – Guidance sensors – Classification of Guidance and Navigation Systems: Basic navigation systems, combined navigation systems – Clas- sification of guidance systems – Three-point tactical guidance laws – Two-point Tactical Guidance Laws: Strategic guidance laws, UAVs guidance laws – Control systems-classical linear time invariant control systems – Transfer function representations – Stability – Time domain characteristics – PID controller design for aerospace systems – Frequency domain characteristics – Root locus – Nyquist and Bode plots and their application to controller design for aerospace systems.

Text Books

Same as Reference

 

References

1. Zarchan, P., Tactical and Strategic Missile Guidance, 4th ed., AIAA (2002).

2. Siouris, G. M., Missile Guidance and Control Systems, AIAA (2004).

3. Titterton, D. H. and Weston, J. L., Strapdown Inertial Navigation Technology, AIAA (2004).

4. Rogers, R. M., Applied Mathematics in Integrated Navigation Systems, 2nd ed., AIAA (2003).

5. Nise, N. S., Control Systems Engineering, Wiley India (2004).

6. Friedland, B., Control System Design, Dover (2005).

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