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Thursday, March 13, 2014

AS7204 SPACECRAFT NAVIGATION SYSTEMS Syllabus

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Anna University Syllabus - Anna University ME Syllabus

AS7204 SPACECRAFT NAVIGATION SYSTEMS Syllabus | Anna University ME Aerospace Technology Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aerospace Technology(Launch Vehicle Technology), Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics. 
It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.


Anna University Chennai Syllabus

AS7204 SPACECRAFT NAVIGATION SYSTEMS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will understand the advanced concepts of Spacecraft
Navigation and to provide the necessary mathematical knowledge that are needed in understanding
their significance and operation. The students will have an exposure on various Navigation systems
such as Inertial Measurement systems, Satellite Navigation – GPS ; and will be able to deploy these
skills effectively in the analysis and understanding of navigation systems in an spacecraft.
UNIT I NAVIGATION CONCEPTS 10
Fundamentals of spacecraft navigation systems and Position Fixing – Geometric concepts of
Navigation – Elements - The Earth in inertial space - Earth's Rotation - Revolution of Earth - Different
Coordinate Systems – Coordinates Transformation - Euler angle formulations - Direction cosine
formulation - Quaternion formulation.
UNIT II GYRO SYSTEMS 8
Gyroscopes -Types – Mechanical - Electromechanical-Optical Gyro -Ring Laser gyro- Fiber optic gyro
- Rate Gyro, Rate Integrating Gyro, Free Gyro, Vertical Gyro, Directional Gyro, Analysis &
Applications
UNIT III INERTIAL NAVIGATION SYSTEMS 10
Accelerometers – Pendulous type – Force Balance type – MEMs Accelerometers - Basic Principles
of Inertial Navigation – Types - Platform and Strap down - Mechanization INS system - Rate
Corrections - Block diagram – Acceleration errors – -Coriolis effect - Schuler Tuning - Cross
coupling - Gimbal lock - Alignment.
UNIT IV GPS & HYBRID NAVIGATION SYSTEMS 9
GPS overview – Concept – GPS Signal – Signal Structure- GPS data – Signal Processing – GPS
Clock – GPS for position and velocity determination – DGPS Concepts - LAAS & WAAS Technology
- Hybrid Navigation - Introduction to Kalman filtering – Case Studies -Integration of GPS and INS
using Kalman Filter.
UNIT V RELATIVE NAVIGATION SYSTEMS 8
Relative Navigation – fundamentals – Equations of Relative Motion for circular orbits
(Clohessy_Wiltshire Equations) - Sensors for Rendezvous Navigation - RF Sensors -Relative
Satellite Navigation - Differential GSP - Relative GPS- Optical rendezvous sensors (Laser type and
Camera type) -Formation Flying - Figure of Merit (FOM)
TOTAL: 45 PERIODS
REFERENCES:
1. Maxwell Noton, ”Spacecraft navigation and guidance”, Springer (London, New York), 1998
2. Slater, J.M. Donnel, C.F.O and others, “Inertial Navigation Analysis and Design”, McGraw-Hill
Book Company, New York, 1964.
3. Albert D. Helfrick, ‘Modern Aviation Electronics’, Second Edition, Prentice Hall Career &
Technology, 1994
4. George M Siouris, ‘Aerospace Avionics System; A Modern Synthesis’, Academic Press Inc., 1993
5. Myron Kyton, Walfred Fried, ‘Avionics Navigation Systems’, John Wiley & Sons, 1997
6. Tsui. J. B.Y, ”Fundamentals of Global Positioning System Receiver”, John Wiley an Sons Inc,

2000

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