Question

1) Flight dynamics and modes of motion a) Determine the state space equations: dx/dt = Ax+Bu; y = Cx; A, B, C: stability derivatives matrices b) Appropriate Transfer Functions by using the new calculated and/or collected data for selected or a new designed type of an aircraft and/or UAV (for example F-16, F-18, F-35 etc) similar to STOL transport aircraft in Appendix B (see Nelson, 2. Ed. etc) using the geometric, mass and aerodynamic characteristics, constant and/or unconstant dominant stability derivatives; c) Investigate the system matrix A: find and discuss the eigenvalues of the matrix; for longitudinal and lateral modes of the aircraft motion. c) Determine the time responses of the airplane for example to a step input of the elevator \(\Delta\delta_e=-0.1 rad\) and/or other appropriate aileron, rudder control surfaces by using MatLab/Simulink. 2) SAS and autopilot design a) Design the autopilot for longitudinal, lateral or directional control system) using inner-outer loop design concept with founded state space equations or transfer functions in 1) a) and b); b) Determine the longitudinal (short and phugoid) and lateral modes time responses to impulse of -10 by using Matlab/Simulink 3) Conclusions and explonations

          1) Flight dynamics and modes of motion
a) Determine the state space equations:
dx/dt = Ax+Bu; y = Cx;
A, B, C: stability derivatives matrices
b) Appropriate Transfer Functions
by using the new calculated and/or collected data for
selected or a new designed type of an aircraft and/or
UAV (for example F-16, F-18, F-35 etc) similar to
STOL transport aircraft in Appendix B (see Nelson,
2. Ed. etc) using the geometric, mass and
aerodynamic characteristics, constant and/or
unconstant dominant stability derivatives;
c) Investigate the system matrix A: find and discuss
the eigenvalues of the matrix; for longitudinal and
lateral modes of the aircraft motion.
c) Determine the time responses of the airplane for
example to a step input of the elevator \(\Delta\delta_e=-0.1 rad\)
and/or other appropriate aileron, rudder control
surfaces by using MatLab/Simulink.
2) SAS and autopilot design
a) Design the autopilot for longitudinal, lateral or
directional control system) using inner-outer loop
design concept with founded state space equations
or transfer functions in 1) a) and b);
b) Determine the longitudinal (short and phugoid)
and lateral modes time responses to impulse of -10
by using Matlab/Simulink
3) Conclusions and explonations

1) Flight dynamics and modes of motion
a) Determine the state space equations:
dx/dt = Ax+Bu; y = Cx;
A, B, C: stability derivatives matrices
b) Appropriate Transfer Functions
by using the new calculated and/or collected data for
selected or a new designed type of an aircraft and/or
UAV (for example F-16, F-18, F-35 etc) similar to
STOL transport aircraft in Appendix B (see Nelson,
2. Ed. etc) using the geometric, mass and
aerodynamic characteristics, constant and/or
unconstant dominant stability derivatives;
c) Investigate the system matrix A: find and discuss
the eigenvalues of the matrix; for longitudinal and
lateral modes of the aircraft motion.
c) Determine the time responses of the airplane for
example to a step input of the elevator Δ=-0.1 rad
and/or other appropriate aileron, rudder control
surfaces by using MatLab/Simulink.
2) SAS and autopilot design
a) Design the autopilot for longitudinal, lateral or
directional control system) using inner-outer loop
design concept with founded state space equations
or transfer functions in 1) a) and b);
b) Determine the longitudinal (short and phugoid)
and lateral modes time responses to impulse of -10
by using Matlab/Simulink
3) Conclusions and explonations

Added by Anthony V.

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