Consider the block diagram of a submersible vehicle shown below: K s+K¡K2 K1 Y(s) R(s) The steady-state tracking error to a unit step input R(s) is Select one: k1 ess k+k2 а. k ess ki+k2 O b. k2 k1(k+k2) ess С. ||
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- (A): Use the Routh-Hurwitz criterion to find the range of (k) for which the system in figure (1) is stable. backsystem, where olowing upuis: 2Juu, 1712u(t) Q2: Awer only Twe Dleel u SIOV in fi GrAP SFG). Reduce the block diagram si nin ure D/S). 519 For TAYA SVStem in * es o wn), percem OVCISIOO 700D settn. g time ( -- MAN R(s) Y(s) 1 1 K s+0.4 2+1.7s+0.25 G1(s) G2(s) G3(s) Figure (1) 0.1 s+0.1 H(s)A 500 MVA synchronous machine has H, = 5.6 MJ/MVA and a 1200 MVA machine has H₂ = 2.0 MJ/MVA. The two machines operate in parallel in a power station. What is the equivalent. H constant for the two, relative to a 100 MVA base?Refer here for the specifications of the D400. a) What power output should you be able to supply from the 24V D400 at 15.4 m/s? b) If the wind drops to 2 m/s, what will the output power be? c) According to the performance graph what is the maximum power you can obtain from the 24V D400? There is a possibility of installing the turbine on top of a 20m high mast instead. Assuming that Zo=0.012, what would you expect the wind speed to be at that height? Use wind shear formula and assume Vref = 7.5 m/s at a height of Zref =10 m.
- 1- Please, Derive Equation of Motion for the 2DOF system with Harmonic force due to the Shaker in the Magnetostrictive Energy Harvesting. Note: I want EOM in Matrices form to get Natural frequencies and mode shapes + Steady-State Response of Spring-Mass System(a) For the system shown in figure find steady state error for (i) Unit step input 10 (ii) Unit Ramp input B)Discuss the effect of the value of K on the system in terms of Percentage overshoot, peak time, settling time, rise time and steady-state error and Use theory to determine the settling time and steady-state error for K = 15 and compare this result with that obtained from the simulation.
- We added the shown Pl controller to reduce the steady-state error of this system to become e=0.1 for a unit ramp input. Determine K that allows us to do that. Hint: start by finding the static velocity constant Kv. KL 19+ R(s) 1 5s + 1 plant controller Select one: O a. 00 O b.9 O d. 10 For the shown system, Use the Routh criterion to deteFmine the range of stability retative to the gain K Note that Kis always positive K> 0. Type a, b, c, d, e or f R(s) C(s) K(s² + s) (s²-2s + 2)(s + 2) byK 1.236 c) 13. The discrete-sme syiem shown in Figure 2 consists of twount-delay elementi and scalar mutiplers. Wite a diftororce equation trat relatos the sutpur ya) and he input ajk]. D D Figure 2.Q4) When the system is subjected to a unit-step input, the system output responds as shown in figure bellow. The maximum overshoot Mp=0.2, find the rise time tr, peak time tp, ,delay time td and settling time ts ? 1.4 1.2 1 0.8 0.6 0.4 0.2 0 1 2 0.2 3 4 5 Time 6 7 8 9 10At one time, three phases symmetrically connected by a proverb, according to the figure on the next slide, are linear currents: Ia 100445° A I, = 1502 – 60° A A) Obtain the symmetric components of linear currents and fuzzy currents. B) Calculate the fuzzy currents passing through the Z impedance. la lab- Ibe leGiven the following unit step response of a second order system, calculate the following values: 1. [ Amplitude 2.1. 3. 32 3 28 28 24 22 2 1.8 1.0 1.4 1.2 1 08 06 04 02 8 Step Response Time (seconds) 10 12 14 the rise time in seconds Tr 15 ] the overshoot in %. Mp. ..] the peak time in seconds Tp.Driving-point admittance The actual impedance of a load is 30 OHM. The per-unit impedance of the load is 0.5 pu when Base Voltage is 600 V and Base Power is of O 6000 VA O 8000 VA O2000 VA 4000 VA Jump to ncements MacBook Air DD DII F10 F9 F8 000 F7 F6SEE MORE QUESTIONS