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Underwater Robots - Gianluca Antonelli.pdf

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XXII Notation<br />

η q =[η T 1 ε T η ] T ∈ IR 7<br />

ν 1 =[u v w ] T ∈ IR 3<br />

ν 2 =[p q r ] T ∈ IR 3<br />

ν =[ν T 1<br />

R β 3 × 3<br />

α ∈ IR<br />

ν T 2 ] T ∈ IR 6<br />

3 × 3<br />

J k,o ( η 2 ) ∈ IR<br />

4 × 3<br />

J k,oq( Q ) ∈ IR<br />

6 × 6<br />

J e ( η 2 ) ∈ IR<br />

7 × 6<br />

J e,q( Q ) ∈ IR<br />

τ 1 =[X Y Z ] T ∈ IR 3<br />

τ 2 =[K M N ] T ∈ IR 3<br />

τ v =[τ T 1<br />

τ � v ∈ IR 6<br />

τ T 2 ] T ∈ IR 6<br />

body(vehicle) position/orientation with the<br />

orientation expressed byquaternions<br />

vector representing the linear velocity ofthe<br />

origin ofthe body(vehicle)-fixed frame with<br />

respect to the origin of the inertial frame expressed<br />

in the body(vehicle)-fixed frame (see<br />

Figure 2.1)<br />

vector representing the angular velocityofthe<br />

body(vehicle)-fixed frame with respect to the<br />

inertial frame expressed in the body(vehicle)fixed<br />

frame (see Figure 2.1)<br />

vector representing the linear/angular velocity<br />

inthe body(vehicle)-fixed frame<br />

rotation matrix expressing the transformation<br />

from frame α to frame β<br />

Jacobian matrix defined in (2.2)<br />

Jacobian matrix defined in (2.10)<br />

Jacobian matrix defined in (2.19)<br />

Jacobian matrix defined in (2.23)<br />

vector representing the resultantforcesacting<br />

on the rigid body(vehicle) expressed in the<br />

body(vehicle)-fixed frame<br />

vector representing the resultant moment acting<br />

on the rigid body(vehicle) expressed in<br />

the body(vehicle)-fixed frame to the pole O b<br />

generalized forces: forces and moments acting<br />

on the vehicle<br />

generalized forces in the earth-fixed-framebased<br />

model defined in (2.53)<br />

n degrees offreedom ofthe manipulator<br />

q ∈ IR n<br />

τ q ∈ IR n<br />

τ =[τ T v<br />

u ∈ IR p<br />

τ T q ] T ∈ IR 6+n<br />

joint positions<br />

joint torques<br />

generalizedforces: vehicle forcesand moments<br />

and joint torques<br />

control inputs, τ = Bu (see (2.72))

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