Control Systems - Part 2 ppt

... variable ω. H igher-Order Systems [Second-order transfer function] Pa g e 67 of 20 9Control S y stems/Print version - Wikibooks, collection of o p en-content textbooks 10/30 /20 06htt p ://en.wikibooks.or g /w/index. p h p ?title =Control _ S y stems/Print _ version& p rintable= y es If ... converges. Pa g e 52 of 20 9Control S y stems/Print version - Wikibooks, collect...

Ngày tải lên: 09/08/2014, 07:20

... -3 .3745×10 20 4.86 3 30.057 468.97 -1 02. 46 -3 .5475×10 K = ⎡⎤ ⎢⎥ ⎣⎦ 39.536 -6 .5518 -2 . 722 9 4.34 02 -2 76.41 173.56 -1 7.953 -2 . 829 K = ⎡ ⎤ ⎢ ⎥ ⎣ ⎦ 3 4.7 321 ×10 859. 72 -1 21 .49 70.976 -5 59.07 664. 62 -9 8. 521 ... = ⎡⎤ ⎢⎥ ⎢⎥ ⎢⎥ ⎣⎦ 1 .22 65 1.5357 -1 .667 -5 .8859 1.5357 2. 5 422 0. 628 9 -5 .1654 -1 .667 0. 628 9 27 .177 30.007...

Ngày tải lên: 21/06/2014, 20:20

...     −       −     HF/ 6-3 1G(d,p) -0 .57 -0 .29 -1 .26 -0 .13 -0 .05 HF/ 6-3 11G(d,p) -0 .55 -0 .30 -1 .13 -0 .14 -0 .06 HF/ 6-3 11++G(d,p) -0 .53 -0 .27 -1 .18 -0 .11 -0 .16 MP2/ 6-3 1G(d,p) -0 . 72 -0 .34 -2 .11 -0 .14 -0 .06 MP2/cc-pVDZ -0 .65 -0 .31 ... D1=C 1 - C 2 -C 3 -C 4 , D2...

Ngày tải lên: 19/06/2014, 11:20

... s αΔT 0 {} s + 0B 11 + B 12 B 11 + B 12 0 ⎡ ⎣ ⎢ ⎤ ⎦ ⎥ a Λ 0 {} (3) κ= E a t s t a + 2t b t a + t a 2 ( ) Λ E s t s 3 12 + E a t s + 2t b () 2 t a 2 + t s + 2t b ()t a 2 + 2 3 t a 3 ⎛ ⎝ ⎜ ⎜ ⎞ ... Conference 20 - 23 April 1998, Long Beach, CA, AIAA, Washington, D.C. 1998, paper no. AIAA-9 8 -2 034. [21 ] Anon., "GBU-39 SDB - Small Diameter Bom...

Ngày tải lên: 19/06/2014, 23:20

... constraints are defined as follows:     20 20  12  12 23 23 23 23  12 25 25       20 20 15 15 17 17 17 17 3 25 25   ( 12)      45 45 45 45 37 37 37 ... control, the sideslip angle is retained virtually at zero. 0 10 20 30 40 −4 2 0 2 t, sec β, deg 0 10 20 30 40 −4 2 0 2 t, sec β, deg 0 10 20 30 40 −4 2 0 2 t, sec β...

Ngày tải lên: 19/06/2014, 23:20

... θ − v b √ V 2 −w 2 b u b √ V 2 −w 2 b 0 w b √ V 2 −v 2 b 0 −u b √ V 2 −v 2 b ⎤ ⎥ ⎥ ⎦ −1 · ⎧ ⎪ ⎪ ⎨ ⎪ ⎪ ⎩ ⎡ ⎣ ν ˙ φ ν ˙ α ν ˙ β ⎤ ⎦ − ⎡ ⎢ ⎢ ⎣ 0 − 1 √ V 2 −w 2 b ( A z + g cos θ cos φ ) 1 √ V 2 −v 2 b  A y + ... 600 −5 0 5 psi 0 20 0 400 600 120 130 140 VTAS 0 20 0 400 600 0 1000 20 00 he 0 20 0 400 600 0 0.1 0 .2 alpha 0 20 0 400 600 −5 0 5 x 10 4 xe 0 20...

Ngày tải lên: 19/06/2014, 23:20

... Gust Failure 0 10 20 30 40 50 60 -2 2 time[s] 0 10 20 30 40 50 60 -2 2 time[s] 0 10 20 30 40 50 60 -2 2 time[s] 0 10 20 30 40 50 60 -2 2 time[s] 0 10 20 30 40 50 60 -2 2 time[s] 1el δ 2el δ 1er δ 2er δ r δ 0 ... 60 -2 2 time[s] 1el δ 2el δ 1er δ 2er δ r δ 0 10 20 30 40 50 60 -2 2 time[s] 0 10 20 30 40 50 60 -2 2 time[s] 0 10 20 30 40 50 60 -2...

Ngày tải lên: 19/06/2014, 23:20

... Flight Control Systems 0 2 4 6 8 10 12 14 16 18 20 20 0 20 40 Bank angle (°) 0 2 4 6 8 10 12 14 16 18 20 24 .5 25 25 .5 26 26 .5 Airspeed (m/s) 0 2 4 6 8 10 12 14 16 18 20 199.9 199.95 20 0 20 0.05 20 0.1 height ... the controls 0 5 10 15 20 25 30 35 40 45 50 20 0 20 Bank angle (°) 0 10 20 30 40 50 60 70 80 24 25 26 27 Airspeed (m/s) 0 20 40 60 8...

Ngày tải lên: 19/06/2014, 23:20

... define the controlled output h 1 in the form of h 1 = C 12 x + D 12 u,where C 12 = ⎡ ⎢ ⎢ ⎣ 0 2 3 3.1 623 0 0 0 3.1 623 0 0 0 1.7 321 ⎤ ⎥ ⎥ ⎦ , D 12 = ⎡ ⎣ 44. 721 4 0 0 28 .28 43 0 3 2 ⎤ ⎦ (13) 24 5 Hierarchical ... 0 1.6349 −58.4053 00 ⎤ ⎦ , E 1 = ⎡ ⎣ −0.5995 −1.38 32 0 ⎤ ⎦ , B 2 = ⎡ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎣ 00 00 00 00 00 00 0.0496 2. 622 4 2. 4 928 0.1740 ⎤ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎦ ,...

Ngày tải lên: 19/06/2014, 23:20

... Control System Fails 28 9 It is easy to see that (40) implies: 22 0 ee AB C D αδαδ ⋅ +⋅ ⋅+⋅ + = (41) where A,B,C,D are given by: () ()() () 2 2 22 2 2 2 2 2 2 2 2 2 2 22 2 2 2 2 2 2 2 2 22 22 ee ... Engineering, 20 , 4 (Oct. 20 07) 21 5- 21 9. ISSN 089 3-1 321 . Kaslik, E.; Balint, A.M.; Chilarescu, C. & Balint, St. (20 02) . The control of...

Ngày tải lên: 19/06/2014, 23:20