一、设计要求
结合本周学习的交流电机原理及启动、调速、制动特性，用Modelica设计和仿真一个用三相交流异步电机带动起重机起升机构运行。具体要求如下：
1）实现如下机械运动周期：控制电机带重物上升，从静止加速到800r/min保持800r/min匀速运动0.5s，减速到静止，保持静止状态0.5s，带重物下降，从静止达到600r/min保持600r/min匀速运动0.6s，减速到静止。(为了便于仿真，匀速和静止持续时间较短)
2) 升降机构和重物折算到到电机转子轴上的等效负载惯量为1Kg.m^2，折算到到电机转子轴上的等效负载转矩是15N.m。
3）使用统一的电机模型,如果控制策略中用到转子串电阻，允许将该电机的转子改为绕线式转子（参数不变）。
4）参照教材中给出的交流电机启动、调速和制动方法，设计控制策略，用Modelica实现控制策略并与电机模型实现联合仿真。
5）可以采用定子串电阻、转子串电阻、定子调压、定子调频等手段，但必须具备工程上的可实施性。
6）评价指标：快速启动、制动，冲击转矩和冲击电流小，能耗小，兼顾实施的经济性。
二、过程分析
本例中采用了自耦变压器降压启动，变频调速，反接制动的方式对交流电机的上述过程进行分析和仿真。
三、参数计算
本例中未给的数据都是通过一次次调试而得到的，没有进行理论计算和推倒，一步步调试的效率比较低，如果可以通过计算得到可以大大提高效率。
四、仿真结果：
代码：
model SACIM "A Simple AC Induction Motor Model"
type Voltage=Real(unit="V");
type Current=Real(unit="A");
type Resistance=Real(unit="Ohm");
type Inductance=Real(unit="H");
type Speed=Real(unit="r/min");
type Torque=Real(unit="N.m");
type Inertia=Real(unit="kg.m^2");
type Frequency=Real(unit="Hz");
type Flux=Real(unit="Wb");
type Angle=Real(unit="rad");
type AngularVelocity=Real(unit="rad/s");
constant Real Pi = 3.1415926;
Current i_A"A Phase Current of Stator";
Current i_B"B Phase Current of Stator";
Current i_C"C Phase Current of Stator";
Voltage u_A"A Phase Voltage of Stator";
Voltage u_B"B Phase Voltage of Stator";
Voltage u_C"C Phase Voltage of Stator";
Current i_a"A Phase Current of Rotor";
Current i_b"B Phase Current of Rotor";
Current i_c"C Phase Current of Rotor";
Frequency f_s"Frequency of Stator";
Torque Tm"Torque of the Motor";
Speed n"Speed of the Motor";
Flux Psi_A"A Phase Flux-Linkage of Stator";
Flux Psi_B"B Phase Flux-Linkage of Stator";
Flux Psi_C"C Phase Flux-Linkage of Stator";
Flux Psi_a"a Phase Flux-Linkage of Rotor";
Flux Psi_b"b Phase Flux-Linkage of Rotor";
Flux Psi_c"c Phase Flux-Linkage of Rotor";
Angle phi"Electrical Angle of Rotor";
Angle phi_m"Mechnical Angle of Rotor";
AngularVelocity w"Angular Velocity of Rotor";
Torque Tl"Load Torque";
Resistance Rs"Stator Resistance";
parameter Resistance Rr=0.408"Rotor Resistance";
parameter Inductance Ls = 0.00252"Stator Leakage Inductance";
parameter Inductance Lr = 0.00252"Rotor Leakage Inductance";
parameter Inductance Lm = 0.00847"Mutual Inductance";
parameter Frequency f_N = 50"Rated Frequency of Stator";
parameter Voltage u_N = 220"Rated Phase Voltage of Stator";
parameter Real p =2"number of pole pairs";
parameter Inertia Jm = 0.1"Motor Inertia";
parameter Inertia Jl = 0.1"Load Inertia";
parameter Real s1=0.5369"frequency rate";
parameter Real s2=0.056"stable frequency rate";
parameter Real s3=0.4026"another frequency rate";
parameter Real P=0.7"stoping rate";
initial equation
Psi_A = 0;
Psi_B = 0;
Psi_C = 0;
Psi_a = 0;
Psi_b = 0;
Psi_c = 0;
phi = 0;
w = 0;
equation
u_A = Rs * i_A + 1000 * der(Psi_A);
u_B = Rs * i_B + 1000 * der(Psi_B);
u_C = Rs * i_C + 1000 * der(Psi_C);
0 = Rr * i_a + 1000 * der(Psi_a);
0 = Rr * i_b + 1000 * der(Psi_b);
0 = Rr * i_c + 1000 * der(Psi_c);
Psi_A = (Lm+Ls)*i_A + (-0.5*Lm)*i_B + (-0.5*Lm)*i_C + (Lm*cos(phi))*i_a + (Lm*cos(phi+2*Pi/3))*i_b + (Lm*cos(phi-2*Pi/3))*i_c;
Psi_B = (-0.5*Lm)*i_A + (Lm+Ls)*i_B + (-0.5*Lm)*i_C + (Lm*cos(phi-2*Pi/3))*i_a + (Lm*cos(phi))*i_b + (Lm*cos(phi+2*Pi/3))*i_c;
Psi_C = (-0.5*Lm)*i_A + (-0.5*Lm)*i_B + (Lm+Ls)*i_C + (Lm*cos(phi+2*Pi/3))*i_a + (Lm*cos(phi-2*Pi/3))*i_b + (Lm*cos(phi))*i_c;
Psi_a = (Lm*cos(phi))*i_A + (Lm*cos(phi-2*Pi/3))*i_B + (Lm*cos(phi+2*Pi/3))*i_C + (Lm+Lr)*i_a + (-0.5*Lm)*i_b + (-0.5*Lm)*i_c;
Psi_b = (Lm*cos(phi+2*Pi/3))*i_A + (Lm*cos(phi))*i_B + (Lm*cos(phi-2*Pi/3))*i_C + (-0.5*Lm)*i_a + (Lm+Lr)*i_b + (-0.5*Lm)*i_c;
Psi_c = (Lm*cos(phi-2*Pi/3))*i_A + (Lm*cos(phi+2*Pi/3))*i_B + (Lm*cos(phi))*i_C + (-0.5*Lm)*i_a + (-0.5*Lm)*i_b + (Lm+Lr)*i_c;
Tm=-p*Lm*((i_A*i_a+i_B*i_b+i_C*i_c)*sin(phi)+(i_A*i_b+i_B*i_c+i_C*i_a)*sin(phi+2*Pi/3)+(i_A*i_c+i_B*i_a+i_C*i_b)*sin(phi-2*Pi/3));
w = 1000 * der(phi_m);
phi_m = phi/p;
n= w*60/(2*Pi);
Tm-Tl = (Jm+Jl) * 1000 * der(w);
Tl = 10;
if time <= 150 then
f_s = 0;
Rs = 0.531;
u_A = 0;
u_B = 0;
u_C = 0;
elseif time<=860 then
f_s = f_N*s1;
Rs = 0.531;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s1;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s1;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s1;
elseif time<=865 then
f_s = f_N*s1;
Rs = 8;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s1;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s1;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s1;
elseif time<=1000 then
f_s = f_N*s1;
Rs = 0.6;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s1;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s1;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s1;
elseif time<=1030then
f_s = f_N*s1;
Rs = 0.531;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s1;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s1;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s1;
elseif time<=1550 then
f_s = f_N*s2;
Rs = 0.531;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s2;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s2;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s2;
elseif time<=1565 then
f_s = f_N*s3;
Rs = 5;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s3;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s3;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s3;
elseif time<=2270 then
f_s = f_N*s3;
Rs = 0.531;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s3;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s3;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s3;
elseif time<=2300 then
f_s = f_N*P*s1;
Rs = 3.5;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s1*P;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s1*P;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s1*P;
elseif time<=2460 then
f_s = f_N*s1;
Rs = 0.531;
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s1;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s1;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s1;
else
u_A = u_N * 1.414 * sin(2*Pi*f_s*time/1000)*s2;
u_B = u_N * 1.414 * sin(2*Pi*f_s*time/1000-2*Pi/3)*s2;
u_C = u_N * 1.414 * sin(2*Pi*f_s*time/1000-4*Pi/3)*s2;
f_s = f_N*s2;
Rs = 0.531;
end if;
end SACIM;
100-300ms加速
300-800ms恒速800r/min
800-1000ms减速
1000-1500ms保持静止
1500-1650ms加速下降
1650-2250ms恒速600r/min
2250-2500ms减速到静止
最终曲线略有波动。
总用时2500ms
仿照蔡瑞东同学的制作。