sesdeactivated
Aerospace
- Oct 28, 2015
- 2
Hi,
Having a bit of trouble with this, assuming a proportional controller is used, I need to determine the gain to achieve a damping ratio of 0.5, for the following transfer function: G(s) = -4(s+0.4) / s^2+1.6s+14.
I need to solve this without using root locus. The furthest I've been able to go is determining the zeros and poles of the transfer function as -0.4, and -1.6+/-3.66i respectively. Some additional data is given: "Data that may be required: (s-2.38)(s+4.14-2.60i)(s+4.14-2.60i)=s^3+5.9s^2+4.24s-56.82" I think I recognise the left hand side of that equation coming from the characteristic equation of a state space model but I'm really not sure how I could use this.
Can anyone lend a hand? Thanks.
Having a bit of trouble with this, assuming a proportional controller is used, I need to determine the gain to achieve a damping ratio of 0.5, for the following transfer function: G(s) = -4(s+0.4) / s^2+1.6s+14.
I need to solve this without using root locus. The furthest I've been able to go is determining the zeros and poles of the transfer function as -0.4, and -1.6+/-3.66i respectively. Some additional data is given: "Data that may be required: (s-2.38)(s+4.14-2.60i)(s+4.14-2.60i)=s^3+5.9s^2+4.24s-56.82" I think I recognise the left hand side of that equation coming from the characteristic equation of a state space model but I'm really not sure how I could use this.
Can anyone lend a hand? Thanks.