| Course title | |||||
| 宇宙制御工学 [Control Engineering in Aerospace] | |||||
| Course category | technology speciality courses,ets. | Requirement | Credit | 2 | |
| Department | Year | 3～4 | Semester | Fall | |
| Course type | Fall | Course code | 023517 | ||
| Instructor(s) | |||||
| 吉村 康広 [] | |||||
| Facility affiliation | Graduate School of Engineering | Office | Email address | ||
| Course description |
|
In this course, you will study the theory and the actual applications of attitude control for spacecraft. The following items are provided. (1)Introduction of the components that are used for attitude control.(2)The theory of the satellite dynamics.(3)The linear control theory. |
| Expected Learning |
|
It is expected to acquire the following ability through this course. (1)Learners are able to recognize the mathematical treatments which used to the attitude control design. (2)Learners are possible to analyze the attitude motion and/or disturbance which affect to space craft on the orbit. (3)Learners will be able to evaluate the performance of the attitude control system. |
| Course schedule |
|
1st; Introductions to the attitude control of satellites and its necessitty. 2nd; Mathematical methodology and the fundamentals of rotational motion 3rd; Satellite dynamics 4th; Satellite kinematics and attitude representations with Euler angles and quaternions 5th; Spin satellite dynamics 6th; Stability analysis of spin satellite dynamics 7th; Disturbances (solar radiation pressure, gravity gradient, and air drag)on satellites, 8th; Mechanism of actuators for satellite attitude control 9th; Sensors for attitude determination and TRIAD method 10th; Gyroscope mathematical model 11th; Sensor fusion and Kalman filter 12th; The difference between classical and modern control theory. 13th; For the simulation, the numerical integration with Runge-kutta method. 14th; Numerical analysis with Runge-Kutta method 15th; Summary and final report |
| Prerequisites |
| The students are expected to have a rudimentary knowledge of Physics, classical control theory, linear algebra |
| Required Text(s) and Materials |
| The original texts which are based the Power point will be prepared. |
| References |
|
Spacecraft Attitude Determination and Control edited by James R. Wertz ISBN 90-277-0959-9 Fundamentals of Spacecraft Attitude Determination and Control,F.Landis Markley, John L. Crassidis, ISBN 1493908014 |
| Assessment/Grading |
| Attendance(20%) and Reports(80%). |
| Message from instructor(s) |
| Course keywords |
| Spacecraft, Attitude control, Satellite dynamics, Satellite kinematics |
| Office hours |
| Remarks 1 |
| Remarks 2 |
| Related URL |
| Lecture Language |
| Language Subject |
| Last update |
| 9/26/2017 3:48:17 PM |