dc.contributor.author |
Thavai, Rahul |
|
dc.contributor.author |
Shaikh, Altamash(12ME48) |
|
dc.contributor.author |
Syed, Adnan (12ME62) |
|
dc.contributor.author |
Padwekar, Aamir(13ME133) |
|
dc.date.accessioned |
2016-08-27T07:35:56Z |
|
dc.date.available |
2016-08-27T07:35:56Z |
|
dc.date.issued |
2016-04-09 |
|
dc.identifier.uri |
http://www.aiktcdspace.org:8080/jspui/handle/123456789/1780 |
|
dc.description |
ICMTEST-16 International Conference on Modern Trends In Engineering, Science And Technology. |
en_US |
dc.description.abstract |
Our project consists of plotting various
outputs of kinematic and dynamic motion with respect to
time . This output is obtained by making a quadcopter to
trace a pescribed trajectory in the MATLAB ra13
simulation platform.the centre of the mass of the
quadcopter is maintained at the centre of the quadcopter
and the following governing kinematic and dynamic
equations are pepared. These equations derived are used
for the inception of the kinematic and dynamic modelling
of the quadcopter made to trace the trajectory. The
outputs of the kinematic and dynamic modelling are made
the input for the correction of error input and tuning of
the PID control system. This closed function PID control
system is used for the stabalization of the quadcopter while
following a given trajectory and optimize the output of the
kinematic and dynamic modelling process for tuning
purpose of the control. Index Terms - List key index
terms here. No mare than 5. |
en_US |
dc.language.iso |
en_US |
en_US |
dc.publisher |
Vishwatmak Om Gurudev College of Engineering |
en_US |
dc.subject |
Staff Publication - SoET |
en_US |
dc.subject |
Staff Publication - ME |
en_US |
dc.subject |
Student Publication - SoET |
en_US |
dc.subject |
Student Publication - ME |
en_US |
dc.title |
Kinematic and Dynamic Modeling of a Quadcopter following a trajectory using MATLAB |
en_US |
dc.type |
Article |
en_US |