AE 245 - Spacecraft Dynamics and Control

Institution:

San Jose State University

Subject:

Description:

Rigid body dynamics review. Attitude kinematical representations. Development and solution of general equations of motion. Single and dual-spin, zero and biased-momentum spacecraft. Control system design strategies. Common torquer elements. Computer simulations. Prerequisite: B S A E or Instructor Consent. 3 units

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.sjsu.edu

Phone Number:

(408) 924-1000

Regional Accreditation:

Western Association of Schools and Colleges

Calendar System:

Semester

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