Variant 10

The longitudinal data for the Foxtrot - a twin – engined, jet fighter / bomber aircraft flying at Mach 0.206 at sea level altitude are given as follows:

U_o=70 m/s;

X_w=0.14; X_u=-0.042; X_q=0; Z_q=-0.76;

Z_w=-0.452; Z_u=-0.177; M_w=-0.006; M_u=-0.0024;

; M_q=-0.317; ; ; ;

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 bomber aircraft and perform the above given task.

Variant 11

The longitudinal data for the Foxtrot - a twin – engined, jet fighter / bomber aircraft flying at Mach 0.9 at 10650 m altitude are given as follows:

U_o=265 m/s;

X_u=-0.009; X_w=0.016; X_q=0; Z_q=-0.88;

Z_w=-0.547; Z_u=-0.088; M_w=-0.03; M_u=-0.008;

; M_q=-0.487; ; ; ;

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 bomber aircraft and perform the above given task.

Variant 12

The longitudinal data for the Foxtrot - a twin – engined, jet fighter / bomber aircraft flying at Mach 1.2 at 10650 m altitude are given as follows:

U_o=350 m/s;

X_u=-0.0135; X_w=0.006; X_q=0; Z_q=-1.25;

Z_w=-0.727; Z_u=0.0125; M_w=-0.08; M_u=0.009;

; M_q=-0.745; ; ; ;

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 bomber aircraft and perform the above given task.

Variant 13

The longitudinal data for the Foxtrot - a twin – engined, jet fighter / bomber aircraft flying at Mach 2.15 at 13700 m altitude are given as follows:

U_o=650 m/s;

X_u=0.016; X_w=0.004; X_q=0; Z_q=-0.39;

Z_w=-0.494; Z_u=-0.001; M_w=-0.07; M_u=0.07;

; M_q=-0.41; ; ; ;

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 bomber aircraft and perform the above given task.

Variant 14

The longitudinal data for the Charlie a very large, four –engined, passenger jet aircraft flying at Mach 0.198 at sea level are given as follows:

U_o=65 m/s;

X_u=-0.021; X_w=0.122; Z_q=-1.9; Z_w=-0.512;

Z_u=-0.2; M_w=-0.006; M_u=0.000036; M_q=-0.357;

; ; ;

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 15

The longitudinal data for the Charlie a very large, four –engined, passenger jet aircraft flying at Mach 0.5 at 6100 m altitude are given as follows:

U_o=158 m/s;

X_u=0.003; X_w=0.078; Z_q=-1.95; Z_w=-0.433;

Z_u=-0.07; M_w=-0.006; M_u=0.00008; M_q=-0.421;

; ; ;

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.