Variant 16
The longitudinal data for the Charlie a very large, four –engined, passenger jet aircraft flying at Mach 0.8 at 6100 m altitude are given as follows:
Uo=250 m/s;
Xu=-0.0002; Xw=0.026; Zq=-3.04; Zw=-0.624;
Zu=-0.09; Mw=-0.005; Mu=-0.00007; Mq=-0.668;
; 
; 
; 
;
The derivatives are not quoted are assumed to be insignificant and are given a zeros value. The state space vector composes the following variables: x=[u w q θ]T
Using state space approach it is necessary to obtain the state space matrices for the Charlie aircraft and perform the above given task.
Variant 17
The longitudinal data for the Charlie a very large, four –engined, passenger jet aircraft flying at Mach 0.8 at 12200 m altitude are given as follows:
Uo=250 m/s;
Xu=0.0002; Xw=0.039; Zq=-1.57; Zw=-0.317;
Zu=-0.07; Mw=-0.003; Mu=-0.00006; Mq=-0.339;
;
; 
; 
;
The derivatives are not quoted are assumed to be insignificant and are given a zeros value. The state space vector composes the following variables: x=[u w q θ]T
Using state space approach it is necessary to obtain the state space matrices for the Charlie aircraft and perform the above given task.
Variant 18
The longitudinal data for the Delta a very large, four –engined, cargo jet aircraft flying at Mach 0.22 at sea level altitude are given as follows:
Uo=75 m/s;
Xu=-0.02; Xw=0.1; Zw=-0.634; Zu=-0.23;
Mw=-0.005; Mu=-2.55x10-5; Mq=-0.61; 
;
; 
; 
;
The derivatives are not quoted are assumed to be insignificant and are given a zeros value. The state space vector composes the following variables: x=[u w q θ]T
Using state space approach it is necessary to obtain the state space matrices for the Delta aircraft and perform the above given task.
Variant 19
The longitudinal data for the Delta a very large, four – engined, cargo jet aircraft flying at Mach 0.6 at 6100m altitude are given as follows:
Uo=190 m/s;
Xu=-0.003; Xw=0.04; Zw=-0.618; Zu=-0.08;
Mw=-0.007; Mu=3.28x10-4; Mq=-0.77; ;
; 
; 
;
The derivatives are not quoted are assumed to be insignificant and are given a zeros value. The state space vector composes the following variables: x=[u w q θ]T
Using state space approach it is necessary to obtain the state space matrices for the Delta aircraft and perform the above given task.