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Computing H ∞ norm of an aircraft dynamics using matlab
V. I. George
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Department of Electrical and Electronics Engineering, Manipal Institute of Technology, Manipal
Manipal Institute of Technology, Manipal
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Engineering
Illustrates
100%
Cruise Condition
100%
Stable Aircraft
100%
Bisection Method
100%
Singular Value
100%
INIS
dynamics
100%
aircraft
100%
norm
100%
values
20%
matrices
20%
calculation methods
20%
Mathematics
Bisection Method
100%
Transfer Matrix
100%
Singular Value
100%
Material Science
Aircraft
100%