Environmental Engineering Reference
In-Depth Information
u dn þ T 2 u dn ¼ v
ð 3 : 36 Þ
v ¼ð k 2 þ g 2 Þ sgn ð s 2 Þ
ð 3 : 37 Þ
where g 2 ¼ max ð T 2 u dn
j
jÞ; T 2 [ 0 ; k 2 [ 0.
3.5.3 q-Axis Current Controller Design
Define an error variable between the required and actual q-axis current:
e 3 ¼ i q i q
ð 3 : 38 Þ
Based on Eq. ( 3.20 ), the q-axis current error dynamics can be expressed by:
e 3 ¼ R
L i q þ xi d þ u q
ð 3 : 39 Þ
L
A TSM manifold is designed as follows [ 12 , 13 ]:
s 3 ¼ e 3 þ c 3 e q 3 = p 3
ð 3 : 40 Þ
3
where c 3 [ 0, p 3 [ 0, q 3 [ 0, p 3 and q 3 are odd.
Theorem 3 If the TSM manifold is chosen as Eq. ( 3.40 ), and the control is
designed as follows, e 3 can converge to zero in finite time [ 25 ]:
u q ¼ u qeq þ u qn
ð 3 : 41 Þ
u qeq ¼ Ri q xLi d Lc 3 e q 3 = p 3
ð 3 : 42 Þ
3
u qn þ T 3 u qn ¼ v
ð 3 : 43 Þ
v ¼ð k 3 þ g 3 Þ sgn ð s 3 Þ
ð 3 : 44 Þ
Þ; T 3 [ 0 ; k 3 [ 0.
where g 3 ¼ max ð T 3 u qn
The proof of Theorems 2 and 3 is similar to that of Theorem 1 and hence is
omitted here.
In Theorem 2 and 3, the control signals, u d and u q , can be transformed to the
control signals s d and s q in Eq. ( 3.12 ) by using the following equations:
Search WWH ::




Custom Search