AV9311 DIGITAL AVIONICS SYLLABUS | ANNA UNIVERSITY ME AVIONICS 1ST SEM SYLLABUS REGULATION 2009 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY FIRST SEMESTER M.E AVIONICS DEPARTMENT SYLLABUS, 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 YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI, TIRUNELVELI,COIMBATORE), 2009 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AV9311 DIGITAL AVIONICS L T P C
3 0 0 3
UNIT I INTRODUCTION TO AVIONICS 4
Role for Avionics in Civil and Military Aircraft systems, Avionics sub-systems and design,
defining avionics System/subsystem requirements-importance of ‘ilities’, Avionics system
architectures.
3
UNIT II AVIONICS SYSTEM DATA BUSES, DESIGN AND INTEGRATION 11
MIL-STD-1553B, ARINC-429, ARINC-629, CSDB, AFDX and its Elements, Avionics system
design, Development and integration-Use of simulation tools, stand alone and integrated
Verification and Validation.
UNIT III AVIONICS SYSTEM ESSENTIALS: DISPLAYS, I/O DEVICES AND POWER
11
Trends in display technology, Alphanumeric displays, character displays etc., Civil and Military
aircraft cockpits, MFDs, MFK, HUD, HDD, HMD, DVI, HOTAS, Synthetic and enhanced
vision, situation awareness, Panoramic/big picture display, virtual cockpit-Civil and Military
Electrical Power requirement standards, comparing the Military and Civil Requirements and
Tips for Power System Design.
UNIT IV PACKAGING 4
Modular Avionics Packaging - Trade-off studies - ARINC and DOD types - system cooling -
EMI/EMC requirements & standards.
UNIT V SYSTEM ASSESSMENT, VALIDATION AND CERTIFICATION 11
Fault tolerant systems - Hardware and Software, Evaluating system design and Future
architecture - Hardware assessment-FARs guide certification requirements-Fault Tree
analysis –Failure mode and effects analysis – Criticality, damaging modes and effects
analysis - Software development process models - Software Assessment and Validation -Civil
and Military standards - Certification of Civil Avionics.
UNIT VI MAINTENANCE and COSTS OF AVIONICS 4
BIT and CFDS, Automatic Test Equipment - Speeds maintenance - ATLAS, Remote
diagnostics and maintenance support-Life Cycle Costs for Military and Civil Avionics - Cash
flow analysis - Software costs - Establishing spares level.
TOTAL : 45 PERIODS
REFERENCES:
1. Spitzer, C.R. “Digital Avionics Systems”, Prentice Hall, Englewood Cliffs, N.J., U.S.A.,
1987.
2. Cary R .Spitzer, “The Avionics Handbook”, CRC Press, 2000.
3. Collinson R.P.G. “Introduction to Avionics”, Chapman and Hall, 1996.
4. Middleton, D.H. “Avionics Systems”, Longman Scientific and Technical, Longman Group
UK Ltd., England, 1989.
5. Jim Curren, “Trend in Advanced Avionics”, IOWA State University, 1992.
AV9311 DIGITAL AVIONICS L T P C
3 0 0 3
UNIT I INTRODUCTION TO AVIONICS 4
Role for Avionics in Civil and Military Aircraft systems, Avionics sub-systems and design,
defining avionics System/subsystem requirements-importance of ‘ilities’, Avionics system
architectures.
3
UNIT II AVIONICS SYSTEM DATA BUSES, DESIGN AND INTEGRATION 11
MIL-STD-1553B, ARINC-429, ARINC-629, CSDB, AFDX and its Elements, Avionics system
design, Development and integration-Use of simulation tools, stand alone and integrated
Verification and Validation.
UNIT III AVIONICS SYSTEM ESSENTIALS: DISPLAYS, I/O DEVICES AND POWER
11
Trends in display technology, Alphanumeric displays, character displays etc., Civil and Military
aircraft cockpits, MFDs, MFK, HUD, HDD, HMD, DVI, HOTAS, Synthetic and enhanced
vision, situation awareness, Panoramic/big picture display, virtual cockpit-Civil and Military
Electrical Power requirement standards, comparing the Military and Civil Requirements and
Tips for Power System Design.
UNIT IV PACKAGING 4
Modular Avionics Packaging - Trade-off studies - ARINC and DOD types - system cooling -
EMI/EMC requirements & standards.
UNIT V SYSTEM ASSESSMENT, VALIDATION AND CERTIFICATION 11
Fault tolerant systems - Hardware and Software, Evaluating system design and Future
architecture - Hardware assessment-FARs guide certification requirements-Fault Tree
analysis –Failure mode and effects analysis – Criticality, damaging modes and effects
analysis - Software development process models - Software Assessment and Validation -Civil
and Military standards - Certification of Civil Avionics.
UNIT VI MAINTENANCE and COSTS OF AVIONICS 4
BIT and CFDS, Automatic Test Equipment - Speeds maintenance - ATLAS, Remote
diagnostics and maintenance support-Life Cycle Costs for Military and Civil Avionics - Cash
flow analysis - Software costs - Establishing spares level.
TOTAL : 45 PERIODS
REFERENCES:
1. Spitzer, C.R. “Digital Avionics Systems”, Prentice Hall, Englewood Cliffs, N.J., U.S.A.,
1987.
2. Cary R .Spitzer, “The Avionics Handbook”, CRC Press, 2000.
3. Collinson R.P.G. “Introduction to Avionics”, Chapman and Hall, 1996.
4. Middleton, D.H. “Avionics Systems”, Longman Scientific and Technical, Longman Group
UK Ltd., England, 1989.
5. Jim Curren, “Trend in Advanced Avionics”, IOWA State University, 1992.
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