Control Systems - Part 6 ppsx

Control Systems - Part 6 ppsx

Control Systems - Part 6 ppsx

... need to be controlled. The task of a control engineer is to design controller and compensator units to interact with these pre-existing systems. However, some systems simply cannot be controlled ... Proportional controller block diagram A Proportional-Derivative controller block diagram Pa g e 158 of 20 9Control S y stems/Print version - Wikibooks, collection of o p en-content te...

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Advances in Flight Control Systems Part 6 pptx

Advances in Flight Control Systems Part 6 pptx

... 400 60 0 −0.1 0 0.1 pbody States 0 200 400 60 0 −1 0 1 phi 0 200 400 60 0 −0.1 0 0.1 qbody 0 200 400 60 0 0 0.1 0.2 theta 0 200 400 60 0 −0.05 0 0.05 rbody 0 200 400 60 0 −5 0 5 psi 0 200 400 60 0 100 150 200 VTAS ... failure 50 55 60 65 70 75 −0.2 −0.1 0 0.1 0.2 C Z & C Z est measured reconstructed 50 55 60 65 70 75 −0.04 −0.02 0 0.02 optimal residual 50 55 60 65...

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Control Systems - Part 8 ppsx

Control Systems - Part 8 ppsx

... License Image:Pierre-Simon-Laplace (174 9-1 827).jpg http://commons.wikimedia.org/wiki/Image:Pierre-Simon-Laplace_(174 9-1 827).jpg Uploaded by commons:User:Luestling Used on Control Systems/ Introduction ... http://commons.wikimedia.org/wiki/Image:Firstorderhold.impulseresponse.svg Uploaded by commons:User:Rbj Public Domain Image:P-controller-symbol-2.svg http://commons.wikimed...

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Mechatronic Systems, Simulation, Modeling and Control 2012 Part 6 pdf

Mechatronic Systems, Simulation, Modeling and Control 2012 Part 6 pdf

... pj  - air resistance load torque j B - viscous-friction coefficient ij K - torque constant j i - armature current j R - armature resistance j u - control input voltage bj K - back-emf ... pj  - air resistance load torque j B - viscous-friction coefficient ij K - torque constant j i - armature current j R - armature res...

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Systems, Structure and Control 2012 Part 6 doc

Systems, Structure and Control 2012 Part 6 doc

... 0.1 360 -0 .2257 0.2 267 k 4 31.5 8.37 39.9 d 2 -3 .79 -3 . 065 9 -2 .2838 k 5 0.5 3.3 0.7 d 3 -3 .33 -3 .333 -2 .5 k 6 -5 .7 -2 3 .6 -1 3.5 e 1 0. 266 5 0.5792 0.4395 k 7 -0 .1 -0 .8 -1 .1 e 2 -0 .7899 -3 .2871 ... 0.3713 h 6 -0 .1 -0 .3 -0 .3 b 3 -0 . 060 1 -0 .0844 -0 .0358 h 7 -3 .2 -2 5.4 -1 2.8 b...

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Corrosion Control Through Organic Coatings Part 6 ppsx

Corrosion Control Through Organic Coatings Part 6 ppsx

... emulsifying, colloid-stabilizing, flash-rust preventing, flow-controlling, thickening, viscosity- controlling, additives, ad infinitum . Examples of unintentional components are cat- alysts or monomer ... of a 4-coat painting scheme, years 6. 1 6. 0 Modified from : Sixth Report of the Corrosion Committee, Spe- cial Report No. 66 , Iron and Steel Institute, London, 1959. 7278_...

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Analysis and Control of Linear Systems - Chapter 6 ppsx

Analysis and Control of Linear Systems - Chapter 6 ppsx

... of a stronger control. 1 76 Analysis and Control of Linear Systems Figure 6. 6. Stabilization by quadratic optimization 166 Analysis and Control of Linear Systems Figure 6. 4. Structure ... ⎟ ⎠ ⎞ ⎜ ⎝ ⎛ = v J 0 and wW = [6. 65] where v and w are positive coefficients. We can verify that () JA, is controllable: () 2 0 rank rank = − = ⎟ ⎠ ⎞ ⎜ ⎝ ⎛ vv v AJJ [6. 66]...

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Robot Motion Planning and Control - J.P. Laumond Part 6 ppsx

Robot Motion Planning and Control - J.P. Laumond Part 6 ppsx

... to 2 2 (0,0,0), with y > -xcot ~, is never optimal. Now, with lemmas 16 to 19 we can remove the part of domains l+l-r -, l+tT_s-r -, t+l-r-r + and l+lTs-rTr + lying out of the first ... by A T the half-line defined as the part of A0 located beyond the point T (with respect to O). According to lemmas 16 to 19, paths l+l-r -, l+lTs-r -, t+l-~rbr +, and l+l~s-r...

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McGraw-Hill- PDA Robotics - Using Your PDA to Control Your Robot 1 Part 6 ppsx

McGraw-Hill- PDA Robotics - Using Your PDA to Control Your Robot 1 Part 6 ppsx

... Bottom .140 .115 .015 .300 .240 .890 .125 .008 .045 .014 .310 5 5 18 .100 .155 .130 .313 .250 .898 .130 .012 .058 .018 .370 10 10 18 2.54 3.94 3.30 7.94 6. 35 22.80 3.30 0.29 1. 46 0. 46 9.40 10 10 .170 .145 .325 . 260 .905 .135 .015 .070 .022 .430 15 15 3. 56 2.92 .038 7 .62 6. 10 22 .61 3.18 0.20 1.14 0. 36 7.87 5 5 4.32 3 .68 8. 26 6 .60 22.99 3.43 0.38 1.78 0. 56 10.92 15 15 n...

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