{VERSION 6 0 "IBM INTEL NT" "6.0" } {USTYLETAB {CSTYLE "Maple Input" -1 0 "Courier" 0 1 255 0 0 1 0 1 0 0 1 0 0 0 0 1 }{CSTYLE "2D Math" -1 2 "Times" 0 1 0 0 0 0 0 0 2 0 0 0 0 0 0 1 }{CSTYLE "2D Comment" 2 18 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 1 } {CSTYLE "" -1 256 "" 1 12 0 0 0 0 0 0 0 0 0 0 0 0 0 1 }{CSTYLE "" -1 257 "" 0 1 0 0 0 0 1 1 0 0 0 0 0 0 0 1 }{PSTYLE "Normal" -1 0 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 }0 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "Text Output" -1 2 1 {CSTYLE "" -1 -1 "Courier " 1 10 0 0 255 1 0 0 0 0 0 1 3 0 3 0 }1 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "Warning" 2 7 1 {CSTYLE "" -1 -1 "" 0 1 0 0 255 1 0 0 0 0 0 0 1 0 0 0 }0 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "Maple Plot" 0 13 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "Normal" -1 256 1 {CSTYLE "" -1 -1 "Times" 1 12 0 0 0 1 2 2 2 2 2 2 1 1 1 1 }3 1 0 0 0 0 1 0 1 0 2 2 0 1 }} {SECT 0 {EXCHG {PARA 0 "" 0 "" {TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT 256 34 "Model for a spaceship around earth" }{TEXT -1 0 "" }}{PARA 0 " " 0 "" {TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 0 "" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 28 "with(plottools):with(plots):" }}{PARA 7 " " 1 "" {TEXT -1 98 "Warning, the previous binding of the name arrow ha s been removed and it now has an assigned value\n" }}}{EXCHG {PARA 0 " > " 0 "" {MPLTEXT 1 0 101 "text:=textplot(\{[0.2,0.1,` earth`],[1.3,2, ` spaceship`],[1,2.1,`(x,y)`],[1.05,1.4,`gravity force`]\}):" }}} {EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 35 "earth:=disk([0,0],0.1,color= BLACK):" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 38 "spaceship:=disk( [1,2],0.03,color=RED):" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 54 "g ravity:=arrow([1,2],[0.8,1.6],.02,.1,.1,color=green):" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 43 "dotline:=line([0,0],[0.8,1.6],lines tyle=2):" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 48 "display(\{text, earth,spaceship,gravity,dotline\});" }}{PARA 13 "" 1 "" {GLPLOT2D 277 234 234 {PLOTDATA 2 "6+-%%TEXTG6$7$$\"\"#!\"\"$\"\"\"F)Q'~earth6\"-F$6 $7$$\"#8F)$F(\"\"!Q+~spaceshipF--F$6$7$$F+F4$\"#@F)Q&(x,y)F--F$6$7$$\" $0\"!\"#$\"#9F)Q.gravity~forceF--%)POLYGONSG6$7U7$F*$F4F47$$\"+8q9@**! 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\"\"F4" }{TEXT -1 2 " " }{XPPEDIT 18 0 "MATRIX([[x], [y]])" "6#-%'MAT RIXG6#7$7#%\"xG7#%\"yG" }}{PARA 0 "" 0 "" {TEXT -1 10 "Canceling " } {XPPEDIT 18 0 "m " "6#%\"mG" }{TEXT -1 27 " from both sides and using \+ " }{XPPEDIT 18 0 "G*M" "6#*&%\"GG\"\"\"%\"MGF%" }{TEXT -1 71 " as unit , we have the simplified model for the trajectory of spaceship:" }} {PARA 0 "" 0 "" {TEXT -1 20 " " }{XPPEDIT 18 0 "MAT RIX([[d^2*x/dt^2], [d^2*y/dt^2]])" "6#-%'MATRIXG6#7$7#*(%\"dG\"\"#%\"x G\"\"\"*$%#dtGF*!\"\"7#*(F)F*%\"yGF,*$F.F*F/" }{TEXT -1 8 " = " } {XPPEDIT 18 0 "-1/sqrt(x^2+y^2)^3" "6#,$*&\"\"\"F%*$-%%sqrtG6#,&*$%\"x G\"\"#F%*$%\"yGF-F%\"\"$!\"\"F1" }{TEXT -1 2 " " }{XPPEDIT 18 0 "MATR IX([[x], [y]])" "6#-%'MATRIXG6#7$7#%\"xG7#%\"yG" }{TEXT -1 10 " \+ (" }{XPPEDIT 18 0 "G*M))" "6#*&%\"GG\"\"\"%\"MGF%" }{TEXT -1 1 ")" } }{PARA 0 "" 0 "" {TEXT -1 50 "Suppose at present, the spaceship is at \+ location (" }{XPPEDIT 18 0 "0,1)" "6$\"\"!\"\"\"" }{TEXT -1 49 ") and \+ moving at speed 0.6 along the direction of " }{XPPEDIT 18 0 "x" "6#%\" xG" }{TEXT -1 48 "-axis, then the IVP of ODE system is as follows:" }} {PARA 0 "" 0 "" {TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 18 " (1) \+ " }{XPPEDIT 18 0 "d^2x/dt^2=-x/sqrt(x^2+y^2)^3" "6#/*(%\"dG\" \"#%\"xG\"\"\"*$%#dtGF&!\"\",$*&F'F(*$-%%sqrtG6#,&*$F'F&F(*$%\"yGF&F( \"\"$F+F+" }{TEXT -1 19 " , " }{XPPEDIT 18 0 "d^2y/dt^ 2=-y/sqrt(x^2+y^2)^3" "6#/*(%\"dG\"\"#%\"yG\"\"\"*$%#dtGF&!\"\",$*&F'F (*$-%%sqrtG6#,&*$%\"xGF&F(*$F'F&F(\"\"$F+F+" }}{PARA 0 "" 0 "" {TEXT -1 20 " " }{XPPEDIT 18 0 "x" "6#%\"xG" }{TEXT -1 15 "(0)=0, " }{XPPEDIT 18 0 "x" "6#%\"xG" }{TEXT -1 32 "'(0)=0 .6, " }{XPPEDIT 18 0 "y" "6#%\"yG" }{TEXT -1 16 "(0)=1, " }{XPPEDIT 18 0 "y" "6#%\"yG" }{TEXT -1 7 "'(0)=0." }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 0 " " }}{PARA 0 "" 0 "" {TEXT -1 120 "This IVP can be solved by Runge-Kutt a program (the process is omitted) and we can plot the trajectory of t he spaceship. 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Solve the 4x4 sy stem, and plot the trajectory." }}{PARA 0 "" 0 "" {TEXT -1 0 "" }} {PARA 0 "" 0 "" {TEXT -1 45 "Homework: The gravity force magnitude i s " }{XPPEDIT 18 0 "G*m*M/(r^s);" "6#**%\"GG\"\"\"%\"mGF%%\"MGF%)%\" rG%\"sG!\"\"" }{TEXT -1 49 " for s = 2. How would the satelite m ove if " }{XPPEDIT 18 0 "s;" "6#%\"sG" }{TEXT -1 2 " i" }{TEXT -1 49 " s different from 2, say, s=1.5, 2.1, 3, etc. " }}{PARA 0 "" 0 "" {TEXT -1 0 "" }}}}{MARK "15 4 5" 44 }{VIEWOPTS 1 1 0 3 2 1804 1 1 1 1 }{PAGENUMBERS 0 1 2 33 1 1 }