ࡱ> SUR9 Rbjbj2V, %l   8Xl'j\\"~~~]]]'''''''$) 6+^9'-]Y]]]9'~~f']~~']'-V!@"~P p]}, m;" "T|'0'G"x+a<+"Ym_l'Yf[xvzu zYef['Y~N0W,g`Q zS2421011_b |*zz*)Yf[b_f[g yf[g-Ne zTyޘLhV[*06R[Nc6Rc-Nee zTyNavigation, Guidance & Control of Aerial VehicleNYe^1Ngs^LyYec]\OS0088198E-mailpli@iipc.zju.edu.cnT|5u݋87951834-806NYe^2lLyoRYec]\OS0097209E-mailbhan@iipc.zju.edu.cnT|5u݋87951834-821Q;`f[epeSvQRM1f[R16f[e 32f[ef[32f[e[vQNf[Rpe28he_fNbՋN0 zQ[-Ne{NN\N300W[ ,g zSbN N NebQ[N0ޘLhV[*|~;NSb1.[*|~i2.`'`[*|~3.s^S`[|~NwcT`[|~4.kSfhQt[MO[*|~5.~T[*|~6.vQ[[*|~7.[*|~vPWhlbcNY`㉗{N0ޘLhVvޘLRRf[^!j;NSb1.ޘLRRf[!jWi2.ޘLhVvޘLRRf[Rg3.ޘLRRf[:gt^!jel4.WNpencvޘLRRf[^!jel5.ޘLRRf[!jWmT^!jel N0ޘLc6R|~NRg1. ޘLhVY`c6RN6R[c6R2. ޘLhVY`c6R{l(1)USVPIDc6R(2)YSϑ&c6R(3)^~'`Y!jWc6R(4)zfc6R3. ޘLhV6R[c6R4. N{|xQWޘLhVޘLc6R|~v~bSvQyr'`5. 6R[Nc6R|~NSOSb/g N0 zQ[Ye{NThis course aims to introduce aircraft navigation, guidance and control technology to enable graduate students with abilities to engage in aircraft control system design and application. The main contents include:1. Aircraft navigation system: platform inertial navigation, strap-down inertial navigation, GPS navigation and integrated navigation etc. will be introduced. The coordinate transformation in navigation and attitude algorithms for navigation system will be discussed. 2. Dynamic model techniques of aircraft: mechanism dynamic modeling, data-based dynamic modeling and hybrid modeling strategy for aircraft.3. Aircraft control system design and analysis: In this part, aircraft attitude control algorithms will be introduced, including single loop PID control, multivariable decoupling control, nonlinear multi-model control and intelligent control etc. At last, the frame and the characteristic of a typical aircraft flight control system will be introduced , and the integrated design technology of guidance and control system will be discussed.V0YwƋbHQO zBl^wQY]yؚI{pef[0ꁨRc6Rt0OSYtI{ebvW@xwƋN0Yef[vvNBlN\N200W[ ,g zO͑N|~҉^[ޘLhVv[*06R[Tc6R|~vۏLN~ e(Wf[u[te*NޘLhVc6RSO| ghQbvƋ0 zQ[mST{|[*|~vN~Tk Sbs^S`[TwcT`[0kSfGPS[*0~T[*I{ޘLhVvRRf[:gt^!j0WNpencv^!jNSmT^!jI{ޘLhVvT{|Y`c6R{lNSޘLhVv6R[c6R0gTNN{|xQWvޘLhVޘLc6R|~v:NOfte*N|~v``Tb]I{0Ǐ,g zvf[`N ggf[uNVQYgevT[(uvޘLhVv[*Tc6RV{euI{ ccޘLc6R|~velTb/g0,g z͑p(WN^(uޘLhV[*Tc6R|~b/g0mQ0YePgbIN~~IN S N @bRvSfNN0SfNv;NSfN1e/cs^ I{W *zzޘLhVޘLRRf[ 024ThXI{W ޘLc6R|~ SN*zz*)Y'Yf[QHr>y 2005t^9g2004t^03y-N 0`'`|~@Nt 0;V2]NQHr>y 1996.74Martin Vermeer: Method of Navigation5wcT`'`[*b/g,{2Hr _)YIQI{ы V2]NQHr>y02007,126. 0ꁨRc6RSt 0,{VHr [~g yf[QHr>y0 kQ0Yef[eScQ[~N~h [0QQvb;N hT!kYef[Q[SbXc0[00ՋI{ Yl1[*6R[c6R[2`'`[*|~3kSf[*T~T[*|~4ޘLRRf[^!jel5ޘLhVY`c6R{l6ޘLhVzfc6RT6R[c6R7[*Nc6R|~NSOSb/g8xQWޘLhVޘLc6R|~N~]N0YlPAGE PAGE 2*4D  2b,. 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