Document information
- University
- Politecnico di Milano
- Degree programme
- Aerospace Engineering
- Subject
- Dynamics and Control of Space Structures
- Classification
- Exercises · By topic
- Original format
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Study material for Dynamics and Control of Space Structures, shared by the Studwiz community and reviewed by moderators.
Study material for Dynamics and Control of Space Structures, shared by the Studwiz community and reviewed by moderators.
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Simply-supported beam F m, EJ, l xs xa l = 0:55 m t = 0:002 m w = 0:05 m = 7700 Kg=m3 E = 200 GPa J = 1 12wt3 m4 xa = 0:7 l xs = 0:4 l – p. 1 Model PLV : Z l 0 v 00T EJv 00 dx = Z l 0 vT mvdx + Z l 0 vT F(t)(x xa)dx Solution : v(x; t) = 1X i=1 i(x)qi(t) = h 1(x) 2(x) ::: i 8 > > < > > : q 1(t) q2(t) ::: 9 > > = > > ; = (x)q(t) i(x) = r 2 ml sin ix l q(t)T Z l 0 00 (x)T EJ 00 (x)dx q(t)+q(t)T Z l 0 (x)T m(x)dx q(t) = q(t)T (xa)T F(t) 00 (x) = h 00 1 (x) 00 2 (x) ::: ::: 00 i (x) ::: ::: i – p. 2 Model M q(t) + Kq(t) = (xa)T F(t) Mij = Z l 0 m i(x) j(x)dx = 2 l Z l 0 sin ix l sin jx l dx = 8 < : 1 i = j 0 i 6= j K ij = Z l 0 EJ 00 i (x) 00 j (x)dx = 2EJ ml i l 2 j l 2 Z l 0 sin ix l sin jx l dx = = 8 < : EJ m i l 4 i = j 0 i 6= j !2 i = EJ m i l 4 – p. 3 Design model qi(t) + !2 i qi(t) = i(xa)F (t) i = 1; 2;:::;np np = number of modes in the design model qi(t) + 2i!i _qi(t) + !2 i qi(t) = i(xa)F (t) i = 1; 2;:::;np i = damping factor of mode i ( = 0:01 ) – p. 4 Design model (state-space) 8 < : _x(t) = A px(t) + Bpu(t) y(t) = Cpx(t) + Dpu(t) x(t) = 8 > > > > > > > > > > > > > > > > < > > > > > > > > > > > > > > > > : q 1(t) _q1(t) q2(t) _q2(t) ::: ::: q np (t) _qnp (t) 9 > > > > > > > > > > > > > > > > = > > > > > > > > > > > > > > > > ; = n ::: ::: q i(t) _qi(t) ::: ::: oT u(t) = F(t) y(t) = v(xs; t) = (xs)q(t) = npX i=1 i(xs)qi(t) – p. 5
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