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#50037 / #1

SoSe 2020 - WiSe 2020/21

English

Spacecraft Dynamics and Control

9

Yoon, Zizung

benotet

Portfolioprüfung

Zugehörigkeit


Fakultät V

Institut für Luft- und Raumfahrt

35341200 FG Raumfahrttechnik

Verkehrswesen

Kontakt


F 6

Yoon, Zizung

zizung.yoon@tu-berlin.de

Learning Outcomes

The module provides the theory and practical application for spacecraft dynamics and control. The students should learn all relevant elements to design and analyze an attitude control system. Thus the goal of the module for the students is to gain theoretical knowledge for spacecrafts attitude control, model dynamic systems and implement the control theory in a real control system.

Content

- Mission analysis and requirements on attitude control systems - Various possibilities of parameterization of spacecraft attitudes - Kinematics of attitude control; Rigid body dynamics - Attitude determination (deterministically, statistically) - Classical control theory (Root locus, PID-controller) - Model-based state prediction - Basics and methods of state control

Module Components

Pflichtgruppe:

All Courses are mandatory.

Course NameTypeNumberCycleLanguageSWSVZ
Spacecraft Dynamics and Control 1VLSoSeEnglish2
Spacecraft Dynamics and Control 2VLWiSeEnglish4

Workload and Credit Points

Spacecraft Dynamics and Control 1 (VL):

Workload descriptionMultiplierHoursTotal
Attendance15.02.0h30.0h
Self-study of lecture materials15.04.0h60.0h
90.0h(~3 LP)

Spacecraft Dynamics and Control 2 (VL):

Workload descriptionMultiplierHoursTotal
Attendance15.04.0h60.0h
Project15.04.0h60.0h
Self-study of lecture materials15.04.0h60.0h
180.0h(~6 LP)
The Workload of the module sums up to 270.0 Hours. Therefore the module contains 9 Credits.

Description of Teaching and Learning Methods

The module consists of lectures, programming exercises, homework and group project work.

Requirements for participation and examination

Desirable prerequisites for participation in the courses:

- Basic knowledge about satellite technologies - Basic knowledge about space flight mechanics

Mandatory requirements for the module test application:

This module has no requirements.

Module completion

Grading

graded

Type of exam

Portfolio examination

Type of portfolio examination

100 Punkte insgesamt

Language

English

Test elements

NamePointsCategorieDuration/Extent
Homework33flexibleNo information
Project34flexibleNo information
Written exam33written60 min

Grading scale

Notenschlüssel »Notenschlüssel 2: Fak IV (2)«

Gesamtpunktzahl1.01.31.72.02.32.73.03.33.74.0
100.0pt95.0pt90.0pt85.0pt80.0pt75.0pt70.0pt65.0pt60.0pt55.0pt50.0pt

Test description (Module completion)

No information

Duration of the Module

The following number of semesters is estimated for taking and completing the module:
2 Semester.

This module may be commenced in the following semesters:
Winter- und Sommersemester.

Maximum Number of Participants

This module is not limited to a number of students.

Registration Procedures

Registration at the MSE secretary according to the MSE study and examination regulations. Dates and deadlines will be announced by semester start.

Recommended reading, Lecture notes

Lecture notes

Availability:  available
Additional information:
The script will be handed out for free in the first lecture.

 

Electronical lecture notes

Availability:  available

 

Literature

Recommended literature
James Wertz, Spacecraft Attitude Determination and Control, Dortrecht 1991
Marcel Sidi, Spacecraft Dynamics and Control, Cambrindge Press, 2000
Peter Berlin, Satelllite Platform Design, Kiruna 2005
Peter Hughes, Spacecraft Attitude Dynamics, Dover Publication Inc, 2004
Wiley Larson, James Wertz, Space Mission Analysis and Design, Dordrecht, 1999

Assigned Degree Programs


This module is used in the following Degree Programs (new System):

Studiengang / StuPOStuPOsVerwendungenErste VerwendungLetzte Verwendung
This module is not used in any degree program.

Miscellaneous

No information