Question 1 (25 marks) Consider the arbitrary characteristic equation: $4 +53 +682 +65 + 7 = 0 (1) Apply the Ruth's crite
Posted: Mon May 09, 2022 9:57 am
Dear Experts,
I sincerely require help to understand how to go about handling
this kinds of question.
Please kindly do not copy and paste from previous questions
posted previously.
A step by step approach and neat hand writing will be
appreciated.
Thank you once again.
Question 1 (25 marks) Consider the arbitrary characteristic equation: $4 +53 +682 +65 + 7 = 0 (1) Apply the Ruth's criteria to evaluate the stability of the system. (8 marks) (ii) Appraise number of roots that are with positive real parts. (2 marks) (6) The following is the small perturbation equation of motion of a DC-8 aircraft, flying at a forward speed of U = 251 m/s. The aircraft is performing an steady level turn with a turn rate: r = 0.0251 rad/s. 0 0 1 -0.0063 1 0 -0.01190 1 0 0 10 V -0.0868 0 -0.0176 -1.18 0.00864 -0.01294 0 1 р -251 0.336 -0.23 0 9.817 0 0 0.0 5.587 -2.11 0.559 132 -0.0519 -1.168113 0 0 φ. (1) Analyse the equation of motion and formulate the simplified equation govering the steady level turn flight. Prove that the equation could be simplified into the following form: 6.6+63 { {*} + = 0 (6 marks) (ii) Hence, or otherwise, appraise the aileron and rudder setting, and the bank angle for the steady level turn flight. (9 marks)
I sincerely require help to understand how to go about handling
this kinds of question.
Please kindly do not copy and paste from previous questions
posted previously.
A step by step approach and neat hand writing will be
appreciated.
Thank you once again.
Question 1 (25 marks) Consider the arbitrary characteristic equation: $4 +53 +682 +65 + 7 = 0 (1) Apply the Ruth's criteria to evaluate the stability of the system. (8 marks) (ii) Appraise number of roots that are with positive real parts. (2 marks) (6) The following is the small perturbation equation of motion of a DC-8 aircraft, flying at a forward speed of U = 251 m/s. The aircraft is performing an steady level turn with a turn rate: r = 0.0251 rad/s. 0 0 1 -0.0063 1 0 -0.01190 1 0 0 10 V -0.0868 0 -0.0176 -1.18 0.00864 -0.01294 0 1 р -251 0.336 -0.23 0 9.817 0 0 0.0 5.587 -2.11 0.559 132 -0.0519 -1.168113 0 0 φ. (1) Analyse the equation of motion and formulate the simplified equation govering the steady level turn flight. Prove that the equation could be simplified into the following form: 6.6+63 { {*} + = 0 (6 marks) (ii) Hence, or otherwise, appraise the aileron and rudder setting, and the bank angle for the steady level turn flight. (9 marks)