Mechatronic Systems, Simulation, Modeling and Control 2012 Part 2 pdf

... Object K C C C Mechatronic Systems, Simulation, Modelling and Control2 6                  2 2 2 6 7 6 5 6 5 6 7 2 2 2 2 2 2 2 2 6 7 6 5 6 5 6 7 6 7 6 5 6 5 6 7 2 2 4 . 6 7 6 5 ... l                 l I (14) I 2 is the 2 2 identity matrix. Hence:   1 2 cos . sin cos 2 sin 2 2 2 2 cos . sin sin 2 cos 2 2 2 2 co 2 2 S md...

Ngày tải lên: 21/06/2014, 11:20

...                                     1 2 2 2 2 2 2 2 2 2 2 2 2 2 2 3 1 2 3 1 2 3 2 K m p p p m a I m a m p p p p x y z a b b x y z (47) The Potential energy ...                                     1 2 2 2 2 2 2 2 2 2 2 2 2 2 2 3 1 2 3 1 2 3 2 K m p p p m a I m a m p p p p x y z a b...

Ngày tải lên: 21/06/2014, 11:20

... (Hall, 20 06; Price, 20 06; Eikenberry, 20 06; Romano & Hall, 20 06; Hall & Romano, 20 07a; Hall & Romano 20 07b). Mechatronic Systems, Simulation, Modelling and Control1 86 Mechatronic Systems, Simulation, Modelling and Control1 82 ... (20 ). From equations of helicopter motion (3)(17) it follows that:       1 1 1 1 3 1 1 1 1 2 cos i G K k K f u I R I  ...

Ngày tải lên: 21/06/2014, 11:20

...      2 2 2 2 2 2 2 2 2 2 2 m a I m a m m g a c a P c P s h H s P c c a b a b x y z                                              2 2 2 3 3 3 3 ... r 2 ( x )  S ( x ) = − 1 d 2 (x)p 4 cos x p3  −d 2 (x) 0 d 1 (x) p 4 cos x p3  0 0 d 3 (x) 1  where ¯ e 1 = −σ 12 ˙ e 1 − σ 11 e 1 ¯ e 2 = −σ 24 e (3) 2 − σ 23 ¨...

Ngày tải lên: 21/06/2014, 11:20

...                                   1 2 1 1 2 2 1 1 2 2 1 1 1 1 2 1 2 2 1 2 1 2 2 2 1 1 2 2 1 1 , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , ...                                   1 2 1 1 2 2 1 1 2 2 1 1 1 1 2 1 2 2 1 2 1 2 2 2 1 1 2 2 1 1 , , , , , , , , , , , , , , , , , ,...

Ngày tải lên: 21/06/2014, 11:20

... position; c) Thruster 2 firing profile; d) Thruster 2 position 1 1 .2 1.4 1.6 1.8 2 2 .2 2.4 2. 6 2. 8 3 1 1 .2 1.4 1.6 1.8 2 2 .2 2.4 2. 6 2. 8 3 X c (m) Y c (m) Actual Commanded t = 46 s t = ... position; c) Thruster 2 firing profile; d) Thruster 2 position 1 1 .2 1.4 1.6 1.8 2 2 .2 2.4 2. 6 2. 8 3 1 1 .2 1.4 1.6 1.8 2 2 .2 2.4 2. 6 2. 8 3 X c (m...

Ngày tải lên: 21/06/2014, 11:20

... (Janocha 20 07). Mechatronic Systems, Simulation, Modelling and Control2 86 Fig. 2. General approach for modelling and testing active flexible micromechanisms 2. 2 Design optimization Modeling, ... d and the stress-free electric Mechatronic Systems, Simulation, Modelling and Control2 90 permittivity matrix ε are each represented by a single coefficient, d 31 and ε 33 res...

Ngày tải lên: 21/06/2014, 11:20

... Mechatronic Systems, Simulation, Modelling and Control2 98 Mechatronic Systems, Simulation, Modelling and Control2 94 3.6 Example of an optimal synthesis ... 439-446, 20 07 Barboni R., and al. (20 00), Optimal placement of PZT actuators for the control of beam dynamics, Smart Material and Structures, pp. 110- 120 , 20 00 Bernardoni P., and al. (20 04a), ... Material and Str...

Ngày tải lên: 21/06/2014, 11:20

... impedance, output impedance, input 1 I Mechatronic Systems, Simulation, Modelling and Control Mechatronic Systems, Simulation, Modelling and Control8 From (27 ), the resonant frequencies can be ... R R n dzrdrdrUm o i 0 2 0 2 )(   , (38)                 h R R EEE n o i dzrdrd r U c r U r U c r U ck 0 2 0 2 2 22 12 2 11 2) (   , (39) dzdr...

Ngày tải lên: 21/06/2014, 07:20

... Replacing eq. (11) in eq. (10) and expanding it the constraint equationࢣ ࢏ is obtained:                 2 2 2 2 2 2 2 c 2 s 2 c 2 c c 2 s 2 c s 0 H a b C C C H C H C H a ... Replacing eq. (11) in eq. (10) and expanding it the constraint equationࢣ ࢏ is obtained:                 2 2 2 2 2 2 2 c 2 s 2 c 2 c c 2 s...

Ngày tải lên: 21/06/2014, 07:20