Model Predictive Control Part 5 pot
... (-10; -5; -10; -5; -1; 0) 4181.6 1370.9 (10; 5; -10; -5; 1; 0) 3322 1406 (10; 5; -10; -5; -1; 0) 157 450 0000 1 452 .1 ( -5; -2; -10; -5; 1; 0) 1411.2 856 .1 (-10; -5; -5; -2; 1; 0) 154 7 .5 850 .9 ... (-10; -5; -10; -5; -1; 0) 4181.6 1370.9 (10; 5; -10; -5; 1; 0) 3322 1406 (10; 5; -10; -5; -1; 0) 157 450 0000 1 452 .1 ( -5; -2; -10; -5; 1; 0) 1411.2 856 .1 (-10; -5; -5; -2; 1;...
Ngày tải lên: 21/06/2014, 03:20
... achieve 77 Distributed Model Predictive Control Based on Dynamic Games Improved Nonlinear Model Predictive Control Based on Genetic Algorithm 57 0 1 2 3 4 5 6 200 250 300 350 400 T, K 0 1 2 3 4 5 6 280 300 320 340 360 380 time, ... J ∗ J ∗ ≤ W max λ min (F ) ( 25) 76 Advanced Model Predictive Control Improved Nonlinear Model Predictive Control B...
Ngày tải lên: 19/06/2014, 19:20
... Multi-dimensional Model Predictive Control for Critical Process with Stochastic Behavior 123 Vojtech Veselý and Danica Rosinová. (2010). Robust Model Predictive Control Design, In: Model Predictive Control, ... k Table 2. Basic fuzzy-neural model unconstrained predictive control algorithm 3.2 Constrained model predictive control The constrained nonlinear p...
Ngày tải lên: 19/06/2014, 19:20
Advanced Model Predictive Control Part 9 pot
... This is the model error when flight mode is changed. 0 5 10 15 20 25 30 35 40 45 50 -2 -1 .5 -1 -0 .5 0 time/s (a) m/s Lateral Velocity in Hovering 0 5 10 15 20 25 30 35 40 45 50 -20 -10 0 10 20 time/s ... s TPP − =⋅−⋅⋅⋅ (A -55 ) () () 2263.28 58 .21 ln wvac vac P λ =−⋅ (A -56 ) () 2 257 .51 85. 95 ln ss P λ =−⋅ (A -57 ) 2 2323.3 4106.7 www HTT=+⋅+ (A -58...
Ngày tải lên: 19/06/2014, 19:20
Advanced Model Predictive Control Part 12 potx
... large-scale model predictive control, in Journal of Process Control, Vol. 12, pp. 7 75 – 7 95. Bemporad, A., & Morari, M. (2004). Robust model predictive control: A survey. In Proc. of European Control ... 300.0 450 .0 0.68 -0.12 5. 48 4 450 (max) TAD1 DE DP inch H2O 1.0 3.9 47.30 -5. 12 9.24 3 controlling Moi TAD1 Gap Prs inch H2O 0.4 1 .5 -0.03 1. 95 0.02 6 0.4 (max...
Ngày tải lên: 19/06/2014, 19:20
Advanced Model Predictive Control Part 13 pot
... discrete-time system (5) is given as (36). A B 1 B 2 C D 1 D 2 = ⎡ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎣ 0.999 65 4.1 350 × 10 −3 −1. 854 4 −0.97 754 0.10639 5. 6762 × 10 −3 0.96481 22.643 −0.07 456 5 −1.3 157 6 .53 86 × 10 5 −3.1960 ... 10 −4 0. 954 23 1.0244 × 10 5 −0.071212 3.2771 × 10 −6 −1.6194 × 10 5 0.097 759 1.0000 −4.1894 × 10 −3 0 0 0 0 0.36788 −0.0 650 04 −0.32122 5. 3617 × 10 −3 5. 256 1 ×...
Ngày tải lên: 19/06/2014, 19:20
Advanced Model Predictive Control Part 14 pot
... 0 10 20 30 40 50 60 70 80 1 47 93 139 1 85 231 277 323 369 4 15 461 50 7 55 3 59 9 6 45 691 737 783 829 Sample Number Percent of Scale Pr o c es s Set Point Actuator Feed Forw ard No Model Adapted Model ... Experimental results 22 .5 2 5. 5 ()et dt⋅ 22 .5 2 5. 5 udtΔ⋅ J Boost pressure overshoot PID+FF 29.11 454 .38 51 .83 34.10 PID+FF+Fuzzy 29.13 2911...
Ngày tải lên: 19/06/2014, 19:20
Advanced Model Predictive Control Part 15 potx
... 3) 0 5 10 15 20 25 30 35 40 6:14 6:21 6:28 6:34 6:41 6:48 6 :54 7:01 7:08 7:14 7:21 7:28 7:34 7:41 7:48 7 :54 8:01 8:08 8:14 8:21 8:28 8:34 8:41 8:48 8 :54 3:26 3:40 3 :53 4:06 4:20 4:33 4:46 5: 00 5: 13 5: 26 5: 40 5: 53 6:06 6:20 6:33 6:46 7:00 7:13 7:26 7:40 10 12 14 16 18 20 22 24 26 28 30 < ... collected at 3 s) BWC - PID Control (Cell 3) 0 0.2 0.4 0.6 0.8 1 1.2 1.4...
Ngày tải lên: 19/06/2014, 19:20
Model Predictive Control Part 5 ppt
... (-10; -5; -10; -5; -1; 0) 4181.6 1370.9 (10; 5; -10; -5; 1; 0) 3322 1406 (10; 5; -10; -5; -1; 0) 157 450 0000 1 452 .1 ( -5; -2; -10; -5; 1; 0) 1411.2 856 .1 (-10; -5; -5; -2; 1; 0) 154 7 .5 850 .9 ... controller GPMN-NMPC (10; 5; 10; 5; 1; 0) 2661.7 1377.0 (10; 5; 10; 5; -1; 0) 3619 .5 13 45. 5 (-10; -5; 10; 5; 1; 0) 2784.9 1388 .5 (-10; -5; 10; 5; -1; 0) 8429.2 1412.0...
Ngày tải lên: 20/06/2014, 11:20
Model Predictive Control Part 15 pot
... exists between -5 0 5 10 -1 0 1 2 3 4 5 il vo -5 0 5 10 1.6 1.8 2 2.2 2.4 2.6 il vo Fig. 2. State partition for N p = 5 (left: whole, rigtht: closeup). Off-line model predictive control of dc-dc ... simulation with a complete aircraft FEA model. Ghiringhelli builds a 13 Model Predictive Control2 74 0 1 2 3 4 5 −0 .5 0 0 .5 1 1 .5 2 2 .5 time [ms] v o [V] 0 1 2 3...
Ngày tải lên: 20/06/2014, 11:20