1.一种具有图像确认的多目标跟踪方法,其特征在于包括下述步骤:
(1)根据所跟踪第i个目标的距离、高低角、方位角、速度、回波信息,高速获取序列图像,通过序列图像处理获得目标的距离、高低角、方位角、速度、回波信息,计算
e=kv(vi-vim)2+kα(αi-αim)2+kβ(βi-βim)2+kr(ri-rim)2
如果e>ed,则该回波不是当前所跟踪的目标;
式中,vi是当前跟踪目标的速度,αi是当前跟踪目标的高低角,βi是当前跟踪目标的方位角,ri是当前跟踪目标斜距,vim是序列图像确定的目标速度,αim是序列图像确定的目标高低角,βim是序列图像确定的目标方位角,rim是序列图像确定的目标斜距,kv,kα,kβ,kr为设定的参数;ed是设定阈值;
(2)所跟踪第i个目标的测量新计算为
式中,xi为9维状态向量,xi=xix·ix··iyiy·iy··iziz·iz··iT,]]>
gi是3、6或9维观测向量,如果雷达只能测量斜距ri、高低角αi、方位角βi时,gi=[riαiβi]T;如果雷达能够测量到速度项,则gi=rir·iαiα·iβiβ·iT;]]>如果雷达能够测量到加速度项,则gi=rir·ir··iαiα·iα··iβiβ·iβ··iT;]]>
式中,下标i代表第i个目标的状态或测量值,
xi(k/k)为第i个目标kT时刻状态的滤波值,
xi(k/k-1)为第i个目标kT时刻状态的一步预测值,
λij(k)为权系数,
gi为观测向量,
zi为gi的实际测量值,
Pi(k/k)为状态估计误差的协方差阵,
Si(k)为新息向量的方差阵,
Ri(k)为观测误差的方差阵,
定义Δi,j(k)为第j个候选回波新息向量,且
Δi,j(k)=zi,j(k)-gi[xi(k/k-1)],
而Δi(k)为Δi,j(k)的加权和,即
Δi(k)=Σj=1mλi,j(k)Δi,j(k),]]>
系数矩阵
p1=xixi2+yi2+zi2]]>
p2=yixi2+yi2+zi2]]>
p3=zixi2+yi2+zi2]]>
p4=-xizi(xi2+yi2+zi2)xi2+yi2]]>
p5=-yizi(xi2+yi2+zi2)xi2+yi2]]>
p6=xi2+yi2(xi2+yi2+zi2)]]>
p7=yixi2+yi2]]>
p8=-xixi2+yi2]]>
h21=x·ixi2+yi2+zi2-xi(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32]]>
h24=y·ixi2+yi2+zi2-yi(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32]]>
h27=z·ixi2+yi2+zi2-zi(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32]]>
h31=x··ixi2+yi2+zi2-xi(x·i2+y·i2+z·i2+xix··i+yiy··i+ziz··i)(xi2+yi2+zi2)32]]>
-2x·i(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32+3xi(xix·i+yiy·i+ziz·i)2(xi2+yi2+zi2)52]]>
h32=2x·ixi2+yi2+zi2-2xi(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32]]>
h34=y··ixi2+yi2+zi2-yi(x·i2+y·i2+z·i2+xix··i+yiy··i+ziz··i)(xi2+yi2+zi2)32]]>
-2y·i(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32+3yi(xix·i+yiy·i+ziz·i)2(xi2+yi2+zi2)52]]>
h35=2y·ixi2+yi2+zi2-2yi(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32]]>
h37=z··ixi2+yi2+zi2-zi(x·i2+y·i2+z·i2+xix··i+yiy··i+ziz··i)(xi2+yi2+zi2)32]]>
-2z·i(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32+3zi(xix·i+yiy·i+ziz·i)2(xi2+yi2+zi2)52]]>
h38=2z·ixi2+yi2+zi2-2zi(xix·i+yiy·i+ziz·i)(xi2+yi2+zi2)32]]>
h51=2xiz·i-x·izi(xi2+yi2+zi2)xi2+yi2-(xi2z·i+yi2z·i-xix·izi-yiy·izi)[xi(xi2+yi2)32(xi2+yi2+zi2)+2xixi2+yi2(xi2+yi2+zi2)2]]]>
h54=2yiz·i-y·izi(xi2+yi2+zi2)xi2+yi2-(xi2z·i+yi2z·i-xix·izi-yiy·izi)[yi(xi2+yi2)32(xi2+yi2+zi2)+2yixi2+yi2(xi2+yi2+zi2)2]]]>
h57=-xix·i+yiy·i(xi2+yi2+zi2)xi2+yi2-(xi2z·i+yi2z·i-xix·izi-yiy·izi)[2zixi2+yi2(xi2+yi2+zi2)2]]]>
h61=x·iz·i-x··izi+2xiz··i(xi2+yi2+zi2)xi2+yi2+(xix·iz·i-x·i2zi-xix··izi+yiy·iz·i-y·i2zi-yiy··izi+xi2z··i+yi2z··i)]]>
[xi(xi2+yi2)32(xi2+yi2+zi2)+2xixi2+yi2(xi2+yi2+zi2)2]]]>
h62=xiz·i+2x·izi(xi2+yi2+zi2)xi2+yi2]]>
h63=-yizi(xi2+yi2+zi2)xi2+yi2]]>
h64=y·iz·i-y·i2zi-y··izi+2yiz··i(xi2+yi2+zi2)xi2+yi2+(xix·iz·i-x·i2zi-xix··izi+yiy·iz·i-y·i2zi-yiy··izi+xi2z··i+yi2z··i)]]>
[yi(xi2+yi2)32(xi2+yi2+zi2)+2yixi2+yi2(xi2+yi2+zi2)2]]]>
h65=yiz·i-2y·izi(xi2+yi2+zi2)xi2+yi2-(xi2z·i+yi2z·i-xix·izi-yiy·izi)[yi(xi2+yi2)32(xi2+yi2+zi2)+2yixi2+yi2(xi2+yi2+zi2)2]]]>
+yizi[xix·i+yiy·i(xi2+yi2)32(xi2+yi2+zi2)+2xix·i+2yiy·i+2ziz·ixi2+yi2(xi2+yi2+zi2)2]]]>
h66=-xizi(xi2+yi2+zi2)xi2+yi2]]>
h67=-x·i2-xix··i-y·i2-yiy··i(xi2+yi2+zi2)xi2+yi2-(xix·iz·i-x·i2zi-xix··izi+yiy·iz·i-y·i2zi-yiy··izi+xi2z··i+yi2z··i)[2zixi2+yi2(xi2+yi2+zi2)2]]]>
+(xix·i+yiy·i)[xix·i+yiy·i(xi2+yi2)32(xi2+yi2+zi2)+2xix·i+2yiy·i+2ziz·ixi2+yi2(xi2+yi2+zi2)2]]]>
+(xi2z·i+yi2z·i-xix·izi-yiy·izi)[2zi(xix·i+yiy·i)(xi2+yi2)32(xi2+yi2+zi2)2-2z·ixi2+yi2(xi2+yi2+zi2)2+4zixi2+yi2(xi2+yi2+zi2)3]]]>
h68=xix·i+yiy·i(xi2+yi2+zi2)xi2+yi2-(xi2z·i+yi2z·i-xix·izi-yiy·izi)[2zixi2+yi2(xi2+yi2+zi2)2]]]>
-(xi2+yi2)[xix·i+yiy·i(xi2+yi2)32(xi2+yi2+zi2)+2xix·i+2yiy·i+2ziz·ixi2+yi2(xi2+yi2+zi2)2]]]>
h69=xi2yi2(xi2+yi2+zi2)xi2+yi2]]>
h81=-y·ixi2+yi2-2xi(x·iyi-xiy·i)(xi2+yi2)2]]>
h84=-x·ixi2+yi2-2yi(x·iyi-xiy·i)(xi2+yi2)2]]>
h91=-y··ixi2+yi2-2xi(x··iyi-xiy··i)(xi2+yi2)2+2y·i(xix·i+yiy·i)-2x·i(x·iyi-xiy·i)(xi2+yi2)2+8xi(x·iyi-xiy·i)(xix·i+yiy·i)(xi2+yi2)3]]>
h92=-2yi(xix·i+yiy·i)+2xi(x·iyi-xiy·i)(xi2+yi2)2]]>
h94=x··ixi2+yi2-2yi(x··iyi-xiy··i)(xi2+yi2)2-2x·i(xix·i+yiy·i)+2y·i(x·iyi-xiy·i)(xi2+yi2)2-8yi(x·iyi-xiy·i)(xix·i+yiy·i)(xi2+yi2)3]]>
h95=-2xi(xix·i+yiy·i)+2yi(x·iyi-xiy·i)(xi2+yi2)3]]>
初始条件为x(0/0);
(3)状态估计的协方差阵为
Pi(k/k)=Pi0(k/k)+Pik(k/k)+Paz+Pal]]>
式中,Paz和Pal分别为雷达转台方位角和高低角转动误差的方差阵,为仅接收到一个回波时状态估计的协方差阵,而定义为:
和Pi(k/k)按照以下原则计算:
当仅接收到一个回波且图像未起作用时,
Pi0(k/k)=Pi0=Pi(k/k-1)-Pi(k/k-1)HiT(k)Si-1(k)Hi(k)Pi(k/k-1)]]>
Pi(k/k)=Pi0+Paz+Pal
当由图像直接确认目标且无相应雷达回波时,协方差与雷达转台无关,则
Pi(k/k)=Pimg_ctr+Pimg_az+Pimg_al
式中,Pimg_ctr为目标中心估计误差的方差阵,Pimg_az为支撑图像系统云台方位角测量误差的方差阵,Pimg_al为支撑图像系统云台高低角测量误差的方差阵;
当由图像直接确认目标且有相应雷达回波时,则
Pi-1(k/k)=(Pimg_ctr+Pimg_az+Pimg_al)-1+(Pi0+Paz+Pal)-1]]>
初始条件为Pi(0/0)。