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Institution:
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Wichita State University
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Subject:
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Aerospace Engineering
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Description:
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AE 707. Modern Flight Control System Design I Modern multi-loop design methods for stability and control augmentation and guidance systems, specifically for aerospace vehicles. State variable model. Optimal state feedback gains and Riccati's equation, tracking systems, sensors and actuator, discretization of continuous dynamic systems, optimal design for digital controls, and effect of non-linearities and trim conditions on design considerations. Prerequisites: AE 514 or 714, and AE 607 or ECE 684 or ME 659.
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Credits:
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3.00
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Credit Hours:
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Prerequisites:
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Corequisites:
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Exclusions:
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Level:
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Instructional Type:
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Lecture
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Notes:
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Additional Information:
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Historical Version(s):
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Institution Website:
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Phone Number:
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(316) 978-3456
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Regional Accreditation:
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North Central Association of Colleges and Schools
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Calendar System:
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Semester
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