A First Course in Differential Equations, Modeling, and Simulation 3rd Edition By Carlos A.
Smith, Scott W. Campbell, Ryan G. Toomey
Chapters 1-11
Chapter 1
Problem 1.1
a)
( ) ( ) ( ) ( ) ( ) ( )
b)
( ) ( ) ( ) ( ) ( ) ( ) ( )
Problem 1.2
a)
w1 (t ) 200 200 u(t 10)
b)
dh
146 166.7 h w1 w2
dt
dh
At the new steady state 0 , therefore,
dt
166.7 h w1 w2 400 100 500
and h 9m
,Problem 1.3
Approximately
20 36 20 36
Thrust t u (t ) (t 0.2)u (t 0.2) t u (t ) (t 0.2)u (t 0.2) 4 u (t 0.4) 4u (t 1)
0.2 0.2 0.2 0.2
CHAPTER 2
Problem 2.1
) ( ) ( )
( ) =>> ∫( )
. /
√
) ( ) ( )
∫ ∫( ( ) ) =>> ( ) ( ( ) )
. / ( )
, ( ) -
) ( )
∫ ∫( ) =>>
, √
) [ ] ( ) ( )
Let with ( )
=>> ∫ ∫ =>>
=>> ∫ ∫( )
( )
( )
) ( ) ( )
[ ]
Let
Then, ( )
∫ ∫ =>>
∫ ∫( ) =>>
) ( )
, ∫ ∫ =>> ( ) =>> ( )
) ( )
∫ ∫ =>> =>>
( ) =>>
) ( ) ( )
( ) =>> ∫ ∫( ) =>> ( ) ( )
( )
. / =>>
) ( )
∫ ∫ =>>
) ( ) ( ) ( )
Let , then
( ) ( )
∫ ∫ ( )