Techniques for aircraft force and moment model development using geometry and stability and control derivative estimates.

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Creator: 

Kaye, Tari Eileen

Date: 

1995

Subject: 

Flight Simulators
Parameter Estimation
Airplanes -- Flight Testing

Language: 

English

Publisher: 

Carleton University

Thesis Degree Name: 

Master of Engineering: 
M.Eng.

Thesis Degree Level: 

Master's

Thesis Degree Discipline: 

Engineering, Mechanical and Aerospace

Parent Collection: 

Theses and Dissertations

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