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Quick Facts
| Medium Of Instructions | Mode Of Learning | Mode Of Delivery |
|---|---|---|
| English | Self Study | Video Based |
Course Overview
The Aircraft Stability and Control programme by Swayam is designed to help the candidates understand what features to include in the aircraft so that it remains statically stable. The online course will cover aircraft manoeuvres extensively and go into the finer details about aircraft flying.
The programme aims to create a solid background for designing an aeroplane from the aspects of stability and control. Swayam’s Aircraft Stability and Control course is a core course intended for undergraduate students, under the category of Aerospace Engineering and Flight Mechanics. Furthermore, this programme will teach them how to introduce specific features in the aircraft so that the pilot can fly the plane at free will.
The Aircraft Stability and Control course by Swayam is an online undergraduate-level course and takes around 12 weeks for completion. This course also provides video lectures and course material, along with weekly assignments and quizzes for self-assessment. Candidates will be able to download or print the reading material for convenient learning.
The Highlights
- 100% Online
- Undergraduate-level course
- Video lectures
- Weekly assignments and quizzes
- No enrolment fees
- E- certificate
- Proctored examination for certification
- Available in regional languages
Programme Offerings
- Downloadable study material
- video lectures
- practice tests
- Proctored examination
- Certificate
- Online discussion forum.
Courses and Certificate Fees
| Fees Informations | Certificate Availability | Certificate Providing Authority |
|---|---|---|
| INR 1000 | yes | IIT Kanpur |
The fees for the course Aircraft Stability and Control is -
| Head | Amount |
| Programme fees | NIL |
| Programme fees (with certificate) | Rs. 1,000 |
Eligibility Criteria
Certificate Qualifying Details
To be eligible for the Aircraft Stability and Control certification, candidates must complete the 12 internal assignments in the course. Of the 12 assignments, the average score of the best eight assignments must be 25% or above. Moreover, candidates also have to take a proctored exam and score at least 75% marks to receive the certificate.
What you will learn
Candidates will be proficient in the following after completing the Aircraft Stability and Control online course successfully:
- Understanding the stability and control aspects of an aircraft
- How to design an aeroplane from the aspect of stability and control
- Features that help a plane stay statically stable
- Detailed knowledge about aircraft stability and control
Who it is for
The Aircraft Stability and Control programme by Swayam is a core course intended for UG students who are interested in learning about how to design an aircraft from stability and control standpoints.
Admission Details
Step 1) Go to the webpage of the Aircraft Stability and Control online course.
Step 2) Enroll in the course by registering with Swayam.
Step 3) To become eligible for certification, fill the examination registration form, the announcements regarding which will be made once the registration process is open.
Step 4) Pay the examination fee and await the publication of your registration form for further details.
The Syllabus
- Overview of aerodynamics and atmosphere
- Wing stall and maximum lift coefficient
- Wing aerodynamic center & pitching moment
- Introduction to static and dynamic stability
- Introduction to static and dynamic stability
- Wing contribution
- Tail contribution
- Canard and fuselage contribution
- Power plant contribution & its effect on NP
- Stick fixed neutral point
- Static margin
- Stick fixed: maneuvering point
- Elevator effectiveness
- Elevator angle of trim
- Flight measurement of Xnp
- Elevator hinge moment
- Stick forces (trim tab & stick force gradient)
- Stick the free neutral point
- Stick free: maneuvering point
- Roll stability and roll control
- Yaw stability and yaw control
- Newton’s second law of rigid dynamics
- Axes system and relevant transforms
- Angular motion equations
- Aerodynamic forces
- Gravitational and thrust forces
- Linearized equations of motion
- Force and moment derivatives
- Contribution of aircraft components to aerodynamic derivatives
- Linear model
- Short period approximation
- Long period approximation
- Pure pitching motion
- Flying and handling qualities
- Linearized lateral dynamics
- Lateral motion: Linearized coupled motion
- Roll approximation
- Spiral approximation
- Dutch roll approximation
- Pure rolling
- Pure yawing
- Inertia coupling
- Stability augmentation system: Longitudinal
- Stability augmentation system: Lateral