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h ˙ = q i n A − g h A R \dot{h}=\frac{q_{in}}{A}-\frac{gh}{AR} h˙=Aqin−ARgh
设 A = 1 A=1 A=1. 目标: h = x → x d h=x\rightarrow x_d h=x→xd —— 保持液面高度
x d = C R g , C = x d g R = u , G ( s ) = 1 S + g R x_d=\frac{CR}{g},C=\frac{x_dg}{R}=u,G\left( s \right) =\frac{1}{S+\frac{g}{R}} xd=gCR,C=Rxdg=u,G(s)=S+Rg1
X = D G 1 + H D G V X=\frac{DG}{1+HDG}V X=1+HDGDGV
明确分析对象
e = T a r g e t − θ e=Target\,\,-\,\,\theta e=Target−θ
Does the error converge to zero or not —— error dynamics stable or not
Open loop 开环
Closed loop 闭环
EG1:
EG2:
G ( s ) = s + 3 s 2 + 2 s + 4 G\left( s \right) =\frac{s+3}{s^2+2s+4} G(s)=s2+2s+4s+3
Matlab可绘制 riocus(g)
掌握根的变化规律 , 设计控制器,补偿器 : Compentator Lead Lag…
根 —— 极点
Matlab可以精确绘制——手绘——掌握根的变化规律——设计控制器
根轨迹的基本形式
根轨迹研究的是: 当 K K K从0到 + ∞ +\infty +∞时,闭环系统根(极点)位置的变化规律
1 + K G ( s ) = 0 , G ( s ) = N ( s ) D ( s ) = ( s − z 1 ) ( s − z 2 ) ⋯ ( s − z m ) ( s − p 1 ) ( s − p 2 ) ⋯ ( s − p n ) 1+KG\left( s \right) =0,G\left( s \right) =\frac{N\left( s \right)}{D\left( s \right)}=\frac{\left( s-z_1 \right) \left( s-z_2 \right) \cdots \left( s-z_{\mathrm{m}} \right)}{\left( s-p_1 \right) \left( s-p_2 \right) \cdots \left( s-p_{\mathrm{n}} \right)} 1+KG(s)=0,G(s)=D(s)N(s)=(s−p1)(s−p2)⋯(s−pn)(s−z1)(s−z2)⋯(s−zm)
其中, z 1 ⋯ z m z_1\cdots z_{\mathrm{m}} z1⋯zm 为零点 Zeros
⊙ \odot ⊙ , p 1 ⋯ p n p_1\cdots p_{\mathrm{n}} p1⋯pn 为极点 Poles
× \times ×
规则1 :共有 n n n条根轨迹, 若 n > m n>m n>m;共有 m m m条根轨迹,若 m > n m>n m>n; ⇐ max { m , n } \Leftarrow \max \left\{ m,n \right\} ⇐max{m,n}
规则2 :若 m = n m=n m=n,随着 K K K从 0 → ∞ 0\rightarrow \infty 0→∞ , 根轨迹从 G ( s ) G\left( s \right) G(s)的极点向零点移动: 1 + K G ( s ) = 0 ⇒ D ( s ) + K N ( s ) = 0 1+KG\left( s \right) =0\Rightarrow D\left( s \right) +KN\left( s \right) =0 1+KG(s)=0⇒D(s)+KN(s)=0 , K → 0 K\rightarrow 0 K→0 时 D ( s ) = 0 D\left( s \right) =0 D(s)=0(极点); K → ∞ K\rightarrow \infty K→∞ 时 N ( s ) = 0 N\left( s \right) =0 N(s)=0 (零点)
规则3:实轴上的根轨迹存在于从右向左第奇数个极点/零点的左边
规则4:若附属跟存在,则一定是共轭的,所以根轨迹通过实轴对称
规则5:若 n > m n>m n>m , 则有 n − m n-m n−m个极点指向无穷;若 m > n m>n m>n , 则有 m − n m-n m−n条根轨迹从无穷指向零点
规则6:根轨迹延渐近线移动,渐近线与实轴的交点 σ = ∑ p − ∑ z n − m \sigma =\frac{\sum{p}-\sum{z}}{n-m} σ=n−m∑p−∑z ,渐近线与实轴的夹角 θ = 2 q + 1 n − m π , q = 0 , 1 , . . . , n − m − 1 / m − n − 1 \theta =\frac{2q+1}{n-m}\pi ,q=0,1,...,n-m-1/m-n-1 θ=n−m2q+1π,q=0,1,...,n−m−1/m−n−1
以 2nd-order system 为例:
Properties of Root locus
G ( s ) = 1 s ( s + 2 ) G\left( s \right) =\frac{1}{s\left( s+2 \right)} G(s)=s(s+2)1
输入Input —— δ ( t ) \delta \left( t \right) δ(t) 单位冲激
——改变根轨迹,希望根在 − 2 + 2 3 -2+2\sqrt{3} −2+23
G ( s ) = 1 s ( s + 2 ) G\left( s \right) =\frac{1}{s\left( s+2 \right)} G(s)=s(s+2)1
在根轨迹上的点满足: ∠ K G ( s ) = − π \angle KG\left( s \right) =-\pi ∠KG(s)=−π (零点到根的夹角和 - 极点到根的夹角和)
H ( s ) = s − z s − p , ∥ z ∥ < ∥ p ∥ H\left( s \right) =\frac{s-z}{s-p},\left\| z \right\| <\left\| p \right\| H(s)=s−ps−z,∥z∥<∥p∥
从稳态误差入手(steady state Error)
误差 Error
: E ( s ) = R ( s ) − X ( s ) = R ( s ) − E ( s ) ⋅ K G ( s ) ⇒ E ( s ) ( 1 + K G ( s ) ) = R ( s ) ⇒ E ( s ) = 1 1 + K G ( s ) R ( s ) = R ( s ) 1 1 + K N ( s ) D ( s ) = 1 s 1 1 + K N ( s ) D ( s ) E\left( s \right) =R\left( s \right) -X\left( s \right) =R\left( s \right) -E\left( s \right) \cdot KG\left( s \right) \Rightarrow E\left( s \right) \left( 1+KG\left( s \right) \right) =R\left( s \right) \Rightarrow E\left( s \right) =\frac{1}{1+KG\left( s \right)}R\left( s \right) =R\left( s \right) \frac{1}{1+K\frac{N\left( s \right)}{D\left( s \right)}}=\frac{1}{s}\frac{1}{1+K\frac{N\left( s \right)}{D\left( s \right)}} E(s)=R(s)−X(s)=R(s)−E(s)⋅KG(s)⇒E(s)(1+KG(s))=R(s)⇒E(s)=1+KG(s)1R(s)=R(s)1+KD(s)N(s)1=s11+KD(s)N(s)1
单位阶跃unit step
: R ( s ) = 1 s R\left( s \right) =\frac{1}{s} R(s)=s1
稳态误差Steady State Error
——FVT终值定理
e s s = lim t → ∞ e ( t ) = lim s → o s E ( s ) = lim s → o s ⋅ 1 s 1 1 + K N ( s ) D ( s ) = 1 1 + K N ( 0 ) D ( 0 ) = D ( 0 ) D ( 0 ) + K N ( 0 ) ess=\underset{t\rightarrow \infty}{\lim}e\left( t \right) =\underset{s\rightarrow o}{\lim}sE\left( s \right) =\underset{s\rightarrow o}{\lim}s\cdot \frac{1}{s}\frac{1}{1+K\frac{N\left( s \right)}{D\left( s \right)}}=\frac{1}{1+K\frac{N\left( 0 \right)}{D\left( 0 \right)}}=\frac{D\left( 0 \right)}{D\left( 0 \right) +KN\left( 0 \right)} ess=t→∞lime(t)=s→olimsE(s)=s→olims⋅s11+KD(s)N(s)1=1+KD(0)N(0)1=D(0)+KN(0)D(0)
P —— Proportional
I —— Integral
D —— Derivative
PID
PD控制:提高稳定性,改善瞬态
PI控制:改善稳态误差
Cauchy’s Argument Priciple 柯西幅角原理
结论: s s s平面内顺时针画一条闭合曲线 A A A, B B B曲线是 A A A通过 F ( s ) F(s) F(s)后在 F ( s ) F(s) F(s)平面上的映射, A A A曲线每包含一个 F ( s ) F(s) F(s)的零点(极点), B B B曲线就绕 ( 0 , 0 ) (0,0) (0,0)点顺时针(逆时针)一圈