### 飞航导弹智能自适应滑模制导律设计

70° TacticalM issile Techno logy January 2006(1) R(1)x2=(-k|R(t)|-R(1))x2- esgm2 (12) (12), R(1)<0 A SMG u (k+1)|R(t)|x2-R(t) gnx2+f 13 L=(k+1)|R(b)1x2-R(1)x1+Esgm2 (14 R(t) A SMg R(t)≈R= const (15) (k+1)|R(1)|x2+ (16 (16), ASMⅥG R(1)△q(1 (9 ,=(k+1)IRI g(t)+ 8sgn q(t).(17) (8) g (t)/l g(t) +81 sgng( t ), 8> f(0)=0(s)>0ifs≠0/(10 (k+1)|R|q(t+E q(1) (18) R()1 RO (18) k= con st> 0 8= const>0 RO R(t)0 (9) R(tx R(1)>0 o1994-2012ChinaAcademicJournalElectronicpUblishingHouse.alLrightsreservedhttp:/www.cnki.net TacticalM issile Techno logy January 2006(1) 71° 噪声 导航计算机知识库 「变结构 导引律 自动驾驶仪 相对运动学模型 1/R 1/5 1/s 4y(7 (y(t)1< 脱靶量 0 5g then let E=Q 18 2)If 0 5g <I ary(t)I< 1g then lete= 3 3 δ=10 (3)Ifk<I ar,(t)|< 1 5g then lete=88 10 ;△y 4)IfI ar,()1>1,, then lete= 12 △ M atlab AR< 1Om 2850m/ (18) △ 08 00 02 1012 15~7, (aAMG 20 K(s)=Ⅱ(s+ (19) 0 (k+1)|R|q(1)+ (s+1) (20 b q(1)|+8 o1994-2012ChinaAcademicJournalelEctronicPublishingHouse.Allrightsreservedhttp://www.cnki.net TacticalM issile Techno logy January 2006(1) /kn R Ro= 3 R= 5 (4(D)d) 0=Q5△y0=1040= 05g PN 22253 26703 534 28l68 4.135 ASMG 2212 265 532 227 256 2.728 PPN 5298 3.83 385 56805 614 8.685 ASMG 5.32 3.85 387 7.8 9.135 C ASMG) PPN 753.2 625.68 121711813946400.7731642 ( PPN ASg 756.15 6289 12231 1664.1 3320.153889 M [MI 2002 200324 (3):245~249 [4 M ario Innocenti Fab i Pellegrin i and Francesco N asuti A VSS Gu dance law fr a gile M issile[ d]. AIAA-97 3473 5 JongkiM oon K iseok K m and Y oud an K im Des gn of M issik gu iance Law vi Var able s tructure Contol[ JI Journal of guidance Control and d ynam ics VoI 24 Na4200k:659~664 [6 Pir Jar Y uan and Jeng-Shing Che m Sohtin ofT ru Propo rtional n av igation for M aneuverng Target[ J] A IA Joumal ofGu dance C ontro I and D ynan ics Vo 15.Na1,1992268~271. o1994-2012ChinaAcademicJournalelEctronicPublishingHouse.Allrightsreservedhttp://www.cnki.net

...展开详情

抢沙发
一个资源只可评论一次，评论内容不能少于5个字
wqq900410

关注 私信 TA的资源

上传资源赚积分,得勋章
最新推荐
飞航导弹智能自适应滑模制导律设计 40积分/C币 立即下载
1/5

试读已结束，剩余3页未读...

40积分/C币 立即下载 ＞