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81. Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives [NASA CR-2200]

by Stepner, David E | Mehra, Raman K.

Material type: book Book; Format: print ; Literary form: not fiction Description: 193p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

82. Stability and control characterstics of a small scale model of an aerial vehicle supported by two ducted fans [NASA TN D-920]

by Parlett, Lysle P.

Material type: book Book Description: 22p.Publisher: Washingtom National aeronautics and space administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

83. Dynamic stability and dispersion of a project mercury test capsule upon entering the atmosphere , with effects of roll rate centre of gravity diplacement, and threshold of a rate reaction control system [NASA TM X-350]

by Jaquet, Byron M.

Material type: book Book; Format: print ; Literary form: not fiction Description: 78p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

84. NASA Technical Note: Longitudinal stability and control derivatives of a Jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation

by Steinmetz, George G | Parrish, Russell V | Bowles, Roland L.

Material type: book Book Description: 43p.Publisher: Washington, D. C. NASA 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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