The rotational velocity ω of the satellite shown in Figure E2.22 is adjusted by changing the length of the beam L. The transfer function between ω(s) and the incremental change in beam length ˆ†L(s) is

The beam length change is ˆ†L(s) = 1/s. Determine the response of the rotation ω(t).

Transcribed Image Text:

2(s 4) (st 5)(s+1): Δ1.(s) Beam adjustuent Rofatinn FIGURE E2.22 Satelite with adjustable rotational velocity.