Type of course: Engineering Science
Prerequisite: Basics of Maths
Rationale: In aircraft it is necessary to control three different types of axis i.e. yaw, pitch and roll. So in order to control such axis it is necessary to understand the basic concepts of control and its detailed theory.
Teaching and Examination Scheme:
Subject Code | Subject Name | L | T | P | Credits | ESE (E) | PA (M) | ESE (V) | PA (I) | Total |
3160104 | Basic Control Theory | 2 | 0 | 2 | 3 | 70 | 30 | 30 | 20 | 150 |
Suggested Specification table with Marks (Theory):
R Level | U Level | A Level | N Level | E Level | C Level |
35% | 25% | 20% | 15% | 5% | 0% |
Legends: R: Remembrance; U: Understanding; A: Application, N: Analyze and E: Evaluate C: Create and above Levels (Revised Bloom’s Taxonomy).
Note: This specification table shall be treated as a general guideline for students and teachers. The actual distribution of marks in the question paper may vary slightly from above table.
Course Outcome:
After learning the course the students should be able to:
- Understand the basic concepts of control systems.
- Know the procedure about how to analyze the problem.
- Design the mathematical model of the system.
- Design the composite types of controllers for any closed loop system.
Major Equipment/Software: MATLAB software or SCILAB or any open source software.
List of Open Source Software: SCILAB.
Learning website: http://nptel.ac.in.
Please find other related topic below.
For Syllabus with Notes Click Here
For List of Experiments/ Practical’s Click Here
For Textbooks or Reference Books Click Here
For Question Papers Click Here
For Question Bank Click Here
For MCQ Quiz Test Series Click Here