AE 243 - Advanced Astrodynamics

Institution:

San Jose State University

Subject:

Description:

Analysis of spacecraft motion using different dynamic models and perturbations. Use of the state transition matrix and differential corrections technique for trajectory computation. Orbit determination and station-keeping methods. Introduction to the three-body problem. Application of computational and analytic methods to solve astrodynamic problems. Prerequisite: A E 242. 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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