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AE 180: Individual Studies
3.00 Credits
San Jose State University
Individual work on special topics. By arrangement. Prerequisites: Upper division standing and Instructor Consent. Repeatable for credit Credit / No Credit 1-3 units
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AE 180 - Individual Studies
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AE 198: Technology and Civilization
3.00 Credits
San Jose State University
See T E C H 198. G E: V 3 units
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AE 198 - Technology and Civilization
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AE 210: Advanced Space Systems Engineering
3.00 Credits
San Jose State University
Overview of the engineering process used in aerospace mission and system design spanning the entire system life cycle for the near- Earth and outer space environment. Effects of gravity field, temperature and radiation on physical systems and the human organism. Mission program inception, proposal development, cost analysis and risk management. Prerequisites: B S A E or Instructor Consent. 3 units
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AE 210 - Advanced Space Systems Engineering
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AE 222: Spacecraft Payload Sensors
3.00 Credits
San Jose State University
Analysis/design of common spacecraft instrumentation and payload sensors. Mission-based characterization of payload sensors including electro-optical, visible, infrared, active/passive R F sensor types. Performance criteria and influence of orbit; computer simulations. Prerequisite: B S A E or Instructor Consent. 3 units
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AE 222 - Spacecraft Payload Sensors
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AE 242: Orbital Mechanics and Mission Design
3.00 Credits
San Jose State University
Two-body problem, conic sections, time of flight. Gibb's method of orbit determination, maneuver analysis for Earth orbiters and interplanetary flight. Euler- Hill equations. Mission design constraints on orbit geometry and launch window analysis. Prerequisite: B S A E or Instructor Consent. 3 units
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AE 242 - Orbital Mechanics and Mission Design
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AE 243: Advanced Astrodynamics
3.00 Credits
San Jose State University
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
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AE 243 - Advanced Astrodynamics
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AE 245: Spacecraft Dynamics and Control
3.00 Credits
San Jose State University
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
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AE 245 - Spacecraft Dynamics and Control
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AE 246: Advanced Aircraft Stability and Control
3.00 Credits
San Jose State University
Natural longitudinal and lateral/directional motion of aircraft; mode shapes, eigenvalues, eigenvectors. Analysis and synthesis of various aircraft autopilots using classical and state space formulations. Prerequisite: B S A E or Instructor Consent. 3 units
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AE 246 - Advanced Aircraft Stability and Control
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AE 250: Advanced Structures and Materials
3.00 Credits
San Jose State University
Design and analysis of modern flight structures including static and dynamic structural response; materials design including metals, alloys, composites. Introduction to modern computational methods including finite elements. Prerequisite: B S A E or Instructor Consent. 3 units
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AE 250 - Advanced Structures and Materials
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AE 262: Advanced Aerodynamics
3.00 Credits
San Jose State University
Thin airfoil theory. Prandtl's lifting-line theory. Subsonic and supersonic airfoil and wing theory. High-angle of attack aerodynamics. Boundary layer theory; Blasius and Falkner- Skan solutions, compressible boundary layers, turbulent flows, separation criteria. Prerequisite: B S A E or Instructor Consent. 3 units
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AE 262 - Advanced Aerodynamics
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