# ps3c - University of Maryland at College Park Dept. of...

This preview shows pages 1–2. Sign up to view the full content.

This preview has intentionally blurred sections. Sign up to view the full version.

View Full Document
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: University of Maryland at College Park Dept. of Aerospace Engineering ENAE 432: Aerospace Control Systems Problem Set #3 Issued: 11 Feb. 2011 Due By: 18 Feb. 2010 You should be able to solve all problems on this homework using only your calculator, pen, and paper. Matlab may be used instead, but only to perform complex number calcu- lations or to find polynomial roots. Any Matlab work must be documented by including a printed diary of the calculations. Any Matlab solution that uses laplace , ilaplace , dsolve , or any other Matlab functionality save for complex number arithmetic and the roots command will be marked incorrect. Any solution in which all calculations are not explicitly documented will be marked incorrect (i.e. you must show all your work). Question 1: A linear system has dynamics governed by the transfer function G ( s ) = s 2 + 5 s + 4 ( s + 2)( s + 3)( s 2 + 2 s + 5) The system has initial conditions y (0) = y (3) (0) = 0, ˙ y (0) = 1, ¨ y (0) =- 1, and is subjected to the input...
View Full Document

## This note was uploaded on 04/07/2012 for the course ENAE 432 taught by Professor Dr.sanner during the Spring '09 term at Maryland.

### Page1 / 2

ps3c - University of Maryland at College Park Dept. of...

This preview shows document pages 1 - 2. Sign up to view the full document.

View Full Document
Ask a homework question - tutors are online