Control Systems Engineering
7th Edition
ISBN: 9781118170519
Author: Norman S. Nise
Publisher: WILEY
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Chapter 3, Problem 10RQ
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Chapter 3 Solutions
Control Systems Engineering
Ch. 3 - Prob. 1RQCh. 3 - State an advantage of the transfer function...Ch. 3 - Define state variables.Ch. 3 - Define state.Ch. 3 - Define state vector.Ch. 3 - Define state space.Ch. 3 - What is required to represent a system in state...Ch. 3 - 8. An eighth-order system would be represented in...Ch. 3 - If the state equations are a system of first-order...Ch. 3 - Prob. 10RQ
Ch. 3 - What factors influence the choice of state...Ch. 3 - What is a convenient choice of state variables for...Ch. 3 - If an electrical network has three energy-storage...Ch. 3 - Prob. 14RQCh. 3 - Prob. 1PCh. 3 - Represent the electrical network shown in Figure...Ch. 3 - Prob. 3PCh. 3 - Represent the system shown in Figure P3.4 in state...Ch. 3 - Represent the rotational mechanical system shown...Ch. 3 - Represent the system shown in Figure P3.7 in state...Ch. 3 - 8. Show that the system of Figure 3.7 in the text...Ch. 3 - Find the state-space representation in...Ch. 3 - MATLAB ML 10. Repeat Problem 9 using MATLAB....Ch. 3 - For each system shown in Figure P3.9, write the...Ch. 3 - MATLAB ML
12. Repeat Problem 11 using MATLAB....Ch. 3 - 13. Represent the following transfer function in...Ch. 3 - Find the transfer function G(s) = Y(s)/R(s) for...Ch. 3 - MATLAB ML
15. Use MATLAB to find the transfer...Ch. 3 - 17. A missile in flight, as shown in Figure P3.10,...Ch. 3 - Given the dc servomotor and load shown in Figure...Ch. 3 - Prob. 20PCh. 3 - Prob. 23PCh. 3 - Experiments to identify precision grip dynamics...Ch. 3 - State-space representations are, in general, not...Ch. 3 - Figure P3.16 shows a schematic description of the...Ch. 3 - Prob. 28PCh. 3 - A single-pole oil cylinder valve contains a spool...Ch. 3 - Figure P3.17 shows a free-body diagram of an...Ch. 3 - 33. Parabolic trough collector. A transfer...
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- A turbine blade made of a metal alloy (k = 17 W/m-K) has a length of 5.3 cm, a perimeter of 11 cm, and a cross-sectional area of 5.13 cm². The turbine blade is exposed to hot gas from the combustion chamber at 1133°C with a convection heat transfer coefficient of 538 W/m²K. The base of the turbine blade maintains a constant temperature of 450°C and the tip is adiabatic. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Hot gas h=538 W/m²K TL E= Turbine blade k = 17 W/m-K p=11 cm, L=5.3 cm A = 5.13cm² T=450°C Determine the temperature at the tip of the turbine blade. The temperature at the tip of the turbine blade is °C.arrow_forward۲/۱ : +0 تا العنوان Ч Example 5.5 The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15, 7.5" above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the Dow rises. h2023-43-115-154 Vees 2V & Pond35. sketch the diagram for them. 147% 3-inpuls RTL-NAND having Re14502 BRO Sel: VIL VBEON 0.65V VIHAVING + 1.34V VHB VIHC Vesss: 1.142V Vine: IB RO+VBES+ 640 Vec Ret 709420 IB₁ 10.3mA Ic: Vec-VCE 5-0-2 Re 45 · 10.67-A ICCE: When A&B &C. "1" Vol No 30206 When A&B &c, "o" Uok Vec5v L.S. 5.06 4.4v VIT 94+114+1.34 -3.42 V N.ML5 V N.Mu-16u T.W= 2.75 169 N.Mu VEM VL N.ML Lex-V Re 16.41A Re ± 10.6mA Pony =69mw 37 L.S >arrow_forwardI don't know how to answer this questionarrow_forward
- Required information Consider a very long, slender rod. One end of the rod is attached to a base surface maintained at Tb, while the surface of the rod is exposed to an air temperature of 400°C. Thermocouples imbedded in the rod at locations 25 mm and 120 mm from the base surface register temperatures of 325°C and 375°C, respectively. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. T₁ Ть T₂ x2 Air Determine the rod length (mm) for the case where the ratio of the heat transfer from a finite length fin to the heat transfer from a very long fin under the same conditions is 99 percent. The length of the rod is mm.arrow_forwardplease find Ix in mm4arrow_forward۲/۱ ∞ + : 5V ON Date AND Loaded with an oR P 5- A R Vect bov V(22)= IR, Vcc-vd 2R V(21) V(22) + Vd=" or V(z) HomeWo Vec-T 022 51-2 العنوان Example 5.5: The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15%, 7.5° above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the Dow rises. Vezi b) V225 V22 lo 21.5 2.15 U 5-0.7 K Loka (I= Vecond R 5:4.57 U 25-0-7 Tak R 5-0.7 5kr V2, Va-IR=5-2.15 -2-85 NEW G C 'WR к >arrow_forward
- : + ♡ +① العنوان I need a detailed drawing with explanation so A 4 ined sove in peaper 96252 Example 5.5 The turbine rotor of ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm ia clockwise direction when viewed from aft. The ship pitches through a total angle of 7.5° above and 7.5° below the horizontal, the motion beingle harmonic and hav gyroscopic couple on the bow rises. ding down be a period of 12 sec. Determine the maximum of the turbine and the direction of yaw as bax r 2.01 ۳/۱arrow_forward88 L Solle ined sove in peaper 96252 Example 5.5 The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15%, 7.5° above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the bow rises. النص ملصقات -20125 750 31 الرسم X 7.0! 989 Carrow_forwardL + ined sove in peaper X-P 96852 Example 5.5 The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15%, 7.5° above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the bow rises. -20125 750 x2.01arrow_forward
- Example 5.5 The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15%, 7.5° above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the bow rises.arrow_forwardPlease explain each step, writing euler rates etcarrow_forward5. (计算题) Calculate the DOF of following mechanisms. If there are compound hinge, passive DOF or Redundant Constraint, please point them out. 品 ⑤A (a) 凸轮拨杆机构arrow_forward
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