control statements part 2

... page as shown in Table 7 -2 135 828 -8 CH07.qxd 136 10/8/07 4 :22 PM Page 136 CHAPTER ■ USING THE ASP.NET AJAX CONTROL TOOLKIT (PART 1) Table 7 -2 AlwaysVisibleControlExtender Control Properties Property ... displayed (see Figure 7- 12)  828 -8 CH07.qxd 10/8/07 4 :22 PM Page 151 CHAPTER ■ USING THE ASP.NET AJAX CONTROL TOOLKIT (PART 1) Figure 7- 12 Selecting a car using CascadingDropDown controls Let’s examine ... 151 828 -8 CH07.qxd 1 52 10/8/07 4 :22 PM Page 1 52 CHAPTER ■ USING THE ASP.NET AJAX CONTROL TOOLKIT (PART 1) Color...

Ngày tải lên: 05/10/2013, 10:20

... TabPanel controls, respectively 20 1 828 -8 CH08.qxd 20 2 10/11/07 10:56 AM Page 20 2 CHAPTER ■ USING THE ASP.NET AJAX CONTROL TOOLKIT (PART 2) Table 8-17 Main Properties of the TabContainer Control ... CH08.qxd 1 92 10/11/07 10:56 AM Page 1 92 CHAPTER ■ USING THE ASP.NET AJAX CONTROL TOOLKIT (PART 2) Figure 8- 12 Rating control being used to rate a person’s preference of Thai food ReorderList Control ... aforementioned code snippet 20 3 828 -8 CH08.qxd 20 4 10/11/07 10:56 AM Page 20 4 CHAPTER ■ USING THE ASP.NET AJAX CONTROL TOOLKIT (PART 2) Figure 8-17 A sample page with a TabContainer control and three TabPanels...

Ngày tải lên: 05/10/2013, 10:20

... http://www.csharp-station.com/Tutorials/Lesson03.aspx 6 /24 /20 02 Tutorial Page of Now that we have a variable in the type we wanted, we will evaluate it with "if" statements The first statement is of the form if (boolean expression) { statements ... this lesson Feedback C# Station Copyright (c) 20 02 C# Station http://www.csharp-station.com/Tutorials/Lesson03.aspx jmayo@csharp-station.com 6 /24 /20 02 ... http://www.csharp-station.com/Tutorials/Lesson03.aspx 6 /24 /20 02 Tutorial Page of statement is optional for the "default" label, as the same behavior will occur without it There are two exceptions to this: adjacent case statements with...

Ngày tải lên: 21/12/2013, 06:16

... evaluates to true, the statements within the curly braces of the "for" loop are executed Normally, these statements http://www.csharp-station.com/Tutorials/Lesson04.aspx 6 /24 /20 02 Tutorial Page of ... this lesson Feedback C# Station Copyright (c) 20 02 C# Station http://www.csharp-station.com/Tutorials/Lesson04.aspx jmayo@csharp-station.com 6 /24 /20 02 ... quit } } Listing 4 -2 shows a "do" loop in action The syntax of the "do" loop is "do { } while ();" The statements can be any valid C# programming statements you like...

Ngày tải lên: 21/12/2013, 06:16

... will be last_int = 21 © 1999 CRC Press LLC num_int = 20 tt_int_ct = 21 0 Thus, the number of integers starting from that would add up to 21 0 is 20 That is, + + + + + 20 = 21 0 3.4 INPUT/OUTPUT ... an analog signal with the following amplitudes: -1 .25 , 2. 57 and 6.0 Solution MATLAB Script diary ex3 _2. dat % y1 = bitatd_3(-1 .25 ) y2 = bitatd_3 (2. 57) y3 = bitatd_3(6.0) diary function Y_dig = bitatd_3(X_analog) ... output y, is represented by the equation: y=0 =1 =2 =3 =4 =5 =6 =7 x < -2. 5 -2. 5 ≤ x < -1.5 -1.5 ≤ x < -0.5 -0.5 ≤ x < 0.5 0.5 ≤ x < 1.5 1.5 ≤ x < 2. 5 2. 5 ≤ x < 3.5 x ≥ 3.5 Write a MATLAB program...

Ngày tải lên: 25/12/2013, 22:15

... use values that are less than 128 The extended character set begins at 128 and continues to 25 5 This program prints all characters between 32 (which is a space) and 25 5 When you run this program, ... simple help system that displays the syntax for the C++ control Help.cpp statements The program displays a menu containing the control statements and then waits for you to choose one After one ... progression 1, 2, 4, 8, 16, 32, and so on 11 The ASCII lowercase letters are separated from the uppercase letters by 32 Thus, to convert a lowercase letter to uppercase, subtract 32 from it Use...

Ngày tải lên: 24/01/2014, 20:20

... use values that are less than 128 The extended character set begins at 128 and continues to 25 5 This program prints all characters between 32 (which is a space) and 25 5 When you run this program, ... simple help system that displays the syntax for the C++ control Help.cpp statements The program displays a menu containing the control statements and then waits for you to choose one After one ... progression 1, 2, 4, 8, 16, 32, and so on 11 The ASCII lowercase letters are separated from the uppercase letters by 32 Thus, to convert a lowercase letter to uppercase, subtract 32 from it Use...

Ngày tải lên: 27/01/2014, 02:20

... use values that are less than 128 The extended character set begins at 128 and continues to 25 5 This program prints all characters between 32 (which is a space) and 25 5 When you run this program, ... simple help system that displays the syntax for the C++ control Help.cpp statements The program displays a menu containing the control statements and then waits for you to choose one After one ... progression 1, 2, 4, 8, 16, 32, and so on 11 The ASCII lowercase letters are separated from the uppercase letters by 32 Thus, to convert a lowercase letter to uppercase, subtract 32 from it Use...

Ngày tải lên: 06/03/2014, 22:20

... ⎥ ⎪ ⎪ ⎪ 11 12 ⎪ ⎥ 2D 66 ⎦CAP ⎩ ⎭ ⎩ ⎭CAP (1) B 12 B 22 B 26 D 12 D 22 D 26 ⎧ Λ⎫ ⎧ (A11 + A 12 )Λ ⎫ 2B16 ⎤ ⎪ ⎥ ⎪ ⎪ ⎪ 2B 26 ⎥ ⎪ Λ⎪ ⎪(A 22 + A 12 )Λ⎪ ⎪ ⎪ ⎪(A16 + A 26 )Λ⎪ 2B 66 ⎥ ⎨ ⎬=⎨ ⎬ ⎥ 2D16 ⎥ ⎪ ⎪ ... ⎣B16 A 12 A 22 A 26 B 12 B 22 B 26 2A16 2A 26 2A 66 2B16 2B 26 2B 66 B11 B 12 B16 D11 D 12 D16 In the late 1980's it was not readily apparent which among the many approaches to adaptive flight control ... adaptive subscale aerospace systems 2 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 Advances in Flight Control Systems Project p=piezoelectric,...

Ngày tải lên: 19/06/2014, 23:20

... al., 20 03, Tsach et al., 20 03, Ren and Beard, 20 04, Wegener et al., 20 04, Ren and Atkins, 20 05, No et al., 20 05, Clough, 20 05, Papadales et al., 20 05, Narasimhan et al., 20 06, Kaminer et al., 20 07) ... the transonic and low supersonic flight speeds .22 ,23 10 Advances in Flight Control Systems Fig GBU-39 Small Diameter Bomb with Adaptive Canards21 2. 2.3 Miniature cruise missile airframe technology ... 1996, Härkegård, 20 03, Farrell et al., Kim et al., 20 04, Shin and Kim, 20 04, Farrell et al., 20 05, Sonneveldt, et al., 20 06, Sonneveldt, et al 20 07)) Most of these designs consider control of the...

Ngày tải lên: 19/06/2014, 23:20

... sin z 12 z 02 + 12 sin z 12 ⎟ − c 13 z13 + Z1 A1ΦT1 ΘF1 + B1 G1 ( X ) − G1 ( X ) + F ⎜ ⎟ c 02 ⎝ ⎠ T T T T des,0 T des,0 ˆ ˆ − Z3 C 3Z3 + + Z1 B1 G1 ( X ) − G1 X − Z2 C Z2 + Z2 A2 ΦT1 ΘF1 + Z2 B2 X ... des Z2 = X − X (28 ) des,0 To stabilize the Z2 subsystem, a virtual feedback control X is defined as des,0 des T ˆ B2 X = −C Z2 − A2 F1 − H + X , C = C > (29 ) des The implementable virtual control ... Eq (38) leads to c 12 T T sin z 12 − c13 z13 − Z2 C Z2 − Z3 C 3Z3 + V − V des,0 z01 + c 02 T des,0 T des,0 T ˆ ˆ z03 + Z1 B1 G1 ( X ) − G1 X + Z2 B2 X − X + Z3 A3 B3 U − U ( 2 V = −c01 z01 − c03...

Ngày tải lên: 19/06/2014, 23:20

... W (20 01), “Tight Formation Control, ” Journal of Guidance, Control, and Dynamics, Vol 24 , No 2, pp 24 6 25 4, doi:10 .25 14 /2. 4735 Wang, J., Patel, V., Cao, C., Hovakimyan, N., and Lavretsky, E (20 08), ... −3.4656 0. 024 5 ⎦ ⎣ Δδe ⎦ −0.0 124 0.0007 2. 29 72 Δδr ⎤ ⎡ ⎤⎡ ⎤ ˙ Δφ p 0.1 024 ⎣ Δ α ⎦ = ⎣ −0.0059 0.9 723 0.0004 ⎦ ⎣ q ⎦ ˙ ˙ Δβ −0.0031 0.00 02 −0.9855 r ⎤⎡ ⎤ ⎡ Δφ 0 + ⎣ 0.0 028 −0.4799 0. 023 5 ⎦ ⎣ Δα ... −1.3568 −0 .26 51 0. 522 0 p ⎣ q ⎦ = ⎣ −0.0655 −0.8947 0.0147 ⎦ ⎣ q ⎦ ˙ ˙ 0.0836 −0.00 42 −0.5135 r r ⎤⎡ ⎡ ⎤ −10.9985 −8.9435 Δφ + ⎣ −0.0007 2. 7041 −0.0064 ⎦ ⎣ Δα ⎦ 0.1841 2. 8 822 Δβ ⎡ ⎤ ⎤⎡ 3 .21 90 −0.0451...

Ngày tải lên: 19/06/2014, 23:20

... Fig 2. 1 Example showing effect of first-order actuator dynamics Let us consider an example with 80.5 2. 6 7.7 20 20 12 12 23 23 23 23 12 25 20 20 15 15 17 17 17 17 25 25 25 45 10 4 .2 0.9 0 .2 4 .2 ... Deflection 2 Direct No Adaptation δr, deg δr, deg 2 −4 −6 2 −4 10 20 t, sec 30 −6 40 10 40 Hybrid RLS Hybrid Indirect δr, deg δr, deg 30 2 2 2 −4 −4 −6 20 t, sec 10 20 t, sec 30 40 −6 10 20 t, ... in Flight Control Systems δe, deg δe, deg −1 2 −3 2 No Adaptation 10 20 t, sec 30 −1 −3 40 10 20 t, sec 10 20 t, sec 30 40 δe, deg δe, deg Direct 0 −1 2 −3 2 Hybrid Indirect 10 20 t, sec...

Ngày tải lên: 19/06/2014, 23:20

... 2 β3 m = 3, , 8} e 2V V pb pb rb rb {α 2V , α 2V , 2 2V , 2 , 2V , βn n = 2, , 5} ¯ pb rb qc 1, β, 2V , 2V , δai , δr i , δspi , {α, V , Ti } m , α qc , αδ , αβ, α 2 , 2 β, αβ3 , 2 ... [m/s] 100 20 0 300 400 500 rbody 0.05 −0.05 140 130 120 100 20 0 300 400 500 20 00 100 20 0 300 400 500 beta 1000 140 130 120 VTAS γ [°] −10 h [m] 0 .2 0.1 0 .2 −0 .2 0 0 20 0 20 0 20 0 20 0 20 0 400 600 ... [m/s] 0.1 −0.1 500 0 .2 0.1 −5 0 20 0 20 0 20 0 400 600 400 600 400 20 0 −3 x 10 600 400 400 20 0 phi 300 theta 20 0 600 600 600 −1 0 .2 0.1 psi 100 400 he 10 20 0 −5 10000 5000 xe 20 0 −5 ye pbody States...

Ngày tải lên: 19/06/2014, 23:20

... VTAS Vtas [m/s] 0. 02 −0. 02 rbody γ [°] −5 0.1 −0.1 0 0 20 0 400 20 0 400 20 0 400 20 0 400 20 0 400 600 600 600 600 600 0 .2 −0 .2 theta 400 600 0 .2 0.1 psi 300 400 −5 he 20 0 20 0 620 600 580 xe 100 −5 ye ... scenario 20 0 400 600 800 1000 120 0 0 .2 0.1 0 20 0 400 600 800 1000 120 0 1400 0.5 −0.5 500 1400 heading [rad] angle of attack [rad] 0 20 0 400 600 800 1000 120 0 1400 20 0 400 600 800 1000 120 0 1400 20 0 ... Flight Control Systems tracking quantities 500 100 20 0 300 400 500 140 130 120 100 20 0 300 400 500 600 100 20 0 300 400 500 0 .2 0.1 0.05 −0.05 beta h [m] 620 580 140 130 120 VTAS Vtas [m/s] 0. 02 −0.02...

Ngày tải lên: 19/06/2014, 23:20

... 50 100 150 20 0 25 0 300 350 50 100 150 20 0 25 0 300 350 50 100 150 20 0 25 0 obs 300 350 350 cmd 50 100 150 20 0 25 0 300 350 25 0 300 350 25 0 300 350 -10 50 100 150 20 0 15 10 0 50 100 150 20 0 time[s] ... 25 0 300 350 50 100 150 20 0 25 0 300 350 50 100 150 20 0 25 0 obs 300 350 350 cmd 50 100 150 20 0 25 0 300 350 25 0 300 350 25 0 300 350 -10 50 100 150 20 0 15 10 0 50 100 150 20 0 time[s] Gust Failure ... 25 0 300 350 50 100 150 20 0 25 0 obs 300 350 350 cmd 50 100 150 20 0 25 0 300 350 25 0 300 350 25 0 300 350 -10 50 100 150 20 0 15 10 0 50 100 150 20 0 time[s] Gust Failure Gust Fig 26 Time history of actuator...

Ngày tải lên: 19/06/2014, 23:20

... Accommodation: Application to a UAV Bank angle (°) 40 20 20 10 15 20 25 30 20 25 30 20 25 30 Airspeed (m/s) 26 .5 26 25 .5 25 24 .5 10 15 height (m) 20 0.1 20 0.05 20 0 199.95 199.9 10 15 time (s) Fig Right ruddervator ... Application to a UAV Bank angle (°) 40 20 20 10 12 14 16 18 20 12 14 16 18 20 12 14 16 18 20 Airspeed (m/s) 26 .5 26 25 .5 25 24 .5 10 height (m) 20 0.1 20 0.05 20 0 199.95 199.9 10 time (s) Fig 10 Left ... fault-tolerant controller Bank angle (°) 10 −10 20 40 60 80 100 120 80 100 120 80 100 120 80 100 120 Airspeed (m/s) 27 26 25 24 20 40 60 height (m) 20 0.5 20 0 199.5 20 40 60 time (s) Sideslip angle (°) 2 20...

Ngày tải lên: 19/06/2014, 23:20

... No 2, pp 21 7 -22 9 Boskovic, J D & Mehra, R K (20 02) , Multiple-Model Adaptive Flight Control Scheme for Accommodation of Actuator Failures, Journal of Guidance, Control, and Dynamics, Vol 25 , No ... and Control, Vol 2, pp 129 5-1300 Kim, K S., Lee, K J & Kim, Y (20 03), Reconfigurable Flight Control System Design Using Direct Adaptive Method, Journal of Guidance, Control, and Dynamics, Vol 26 , ... perturbations Partially differentiating equation (18) with respect to the velocity magnitude yields the desired result, ∂C W ∂ −qSC L − ρVSC L C = ≈ =2 W m ∂V ∂V m V (22 ) Combining equations (20 ) to (22 )...

Ngày tải lên: 19/06/2014, 23:20

... 60] [m/s] 20 0 Advances in Flight Control Systems u [m/s] w [m/s] 60 2 40 −4 −6 20 −8 0 20 40 60 −10 20 θ [deg] 40 60 40 60 40 60 λ i 0.06 2 0.04 −4 −6 0. 02 −8 −10 20 V [m/s] 40 60 0 20 V [m/s] ... McClamroch, N.H (20 02) Aggressive longitudinal aircraft trajectory tracking using nonlinear control Journal of Guidance, Control and Dynamics, Vol 25 , No 1, January 20 02, pp 26 – 32, ISSN 07315090 ... [1/rad] c 0 .27 [m] m 22 00 [kg] Ibl 23 1.7 [kgm2 ] Iyy 4973.0 [kgm2 ] R 4.91 [m] Ω 44.4 [rad/s] N [-] CD S 1.5 [m2 ] hR 1.48 [m] Table Parameters of Bo105 (Padfield, 1996) Vr Vc1 Vc2 tc1 tc2 tc3 tc4...

Ngày tải lên: 19/06/2014, 23:20

... camera z2 = D1 ⋅ z1 D2 (9) x2 = X2 ⋅ z2 f (10) y2 = Y2 ⋅ z2 f (11) Camera coordinate D1 D2 X Camera coordinate D1 Y X (Xc1,Yc1) (Xc2,Yc2) f Y f (Xc1,Yc1) z2 y z z1 (x1,y1) (x1,y1) y (x2,y2) d1 ... 20 8 Advances in Flight Control Systems H cost 2. 4 F fix−3 2. 3 Fgs−1 2. 2 Fgs−3 Fgs 2 2.1 1.9 1.8 1.7 10 20 V [m/s] 30 40 50 Fig H2 cost 5.1 Evaluation of design ... 150 θ [deg] 20 15 c θ [deg] 25 50 10 0 50 t [s] 100 2 150 50 t [s] (a) Controlled variables and inputs Fixed−SF 20 00 e x [m] 3000 1000 0 20 40 60 20 40 60 t [s] 80 100 120 140 80 100 120 140 100...

Ngày tải lên: 19/06/2014, 23:20