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1 14 BIRD 1. ALOS ETS ETS- 6 6 ETS- 2 ETS- 3 ETS
2 SN kg 500mm H-A 2 H-A 5 H-A JIS C Hz ETS Hz kg 450R380P500Y mm 450R3110 P500Ymm mm km deg
3 BIRD 50kg H-A km 35deg sec 450R 380P 500Ymm 450R 3110P 500Ymm MHz 0.5kbps 2250MHz 20kbps 300kbps Hz 0.66Hz 1 16 MSC. Nastran Al 25mm Hz Hz 2.0kg Al 6 2mm Al Hz 0.66Hz 3 5.5kg Al 6 Al Al C&DH 7 2.6
4 2.2 sec sec sec days C&DH CPU JIS 2 JIS 2 4
5 2.3 Al Al GPa kg/m JIS 7 JIS 1 JIS f f 1 = e kt 3.1 f f 1 k T f f 2 2 f 2 T = log e 3.2 k f1 5 1 T=1f=2f k = log e t t = 120 log 10 log 2 10 f f log 10 f f OBC 10
6 0.36Hz 0.35Hz 35Hz Hz 2.635Hz JIS A-setB-setC-setD-set JIS JIS A-set 3.2 B-set 3.3 C-set 3.4 D-set 3.1 f 2 / f 1 sec Hz Hz
7 Hz Hz rad/s Rm mkg
8 3.6 Z Z X X 3.6 A-set B-setC-setD-set A-setB-setC-setD-set X X X A-set B-set 2 3 C-set 1 3 D-set A-setB-setC-setD-set 3 0 A-set 1 2 B-set 2 C-set 1 X F = 2mRω sinωt a ACC 5% 8Gm/s 2 5% a ACC a ACC = = m/s x ACC u ACC = x sinωt 3.7 ACC 2 x ACC a ACC = ω sin ωt 1 ACC 1 VM x VM x VM φvm φvm a ACC = x ACC = φ φ ω sinωt ACC ACC u VM x VM M F VM 2 = Mu&& = Mx ω sin ωt = Ma VM ACC φ φ VM ACC VM 3.10 F VM m R 3 1 8
9 3.7 A-set A-set A-set B-set B-set B-set C-set C-set C-set D-set D-set D-set st 2nd 3rd A-set B-set C-set D-set sint=1 M=50kg3.6 a ACC F VM = Ma ACC = = N DANAHER MOTION QT 9 9
10 A/D NASAJAXA Silicon Designs Silicon Designs JAXA OBC Guyan 12 Guyan i K ii i M ii K ii R i = 3.12 M ii 1 =K/M 1/2 R i R i mg Rm Hz Hz N N Nm QT-2105 QT-1406 Nm Hz g m m m
11 3.6 Model mm /125 m/s 2 2G Hz 0400 g 10 m/s 2 8G 3.7 NR-2000 NR-2010 mm /50 0/ g khz A/D bit A B A 1 Guyan 12 1 B A Guyan B Guyan Guyan
12 Guyan Guyan MAC MAC i i j j ( ) T 2 { φi } { φ j } T T ({ φ } { φ }){ ( φ } { φ }) MAC ij = 3.13 i i j MAC MAC MAC MAC 0 j MAC Guyan Guyan 9 10 MAC Guyan Guyan
13 3.27 MACGuyan 3.28 MAC 3.29 MACGuyan 3.30 MAC ETS- Eigensystem Realization AlgorithmERA 3 ETS-ERA Extended Kalman FilterEKF Hz 2.635Hz 5% MSC.Nastran 5% 5% Hz
14 % D-set X A-set Hz 5 A-set 2.635Hz 5 B-set Hz 5 2. JIS B-set 2.635Hz 5 C-set Hz C-set 2.635Hz 5 D-set Hz 3 D-set 2.635Hz Hz Hz Hz Hz Hz Hz Hz Hz Hz
15 3.9 sec ON GO/NOGO OFF ON GO/NOGO GO JIS 450 OFF GO/NOGO OBC OBC
16 OBC OBC C&DH R380P500Ymm mm Al 5 Al Al Al RPY= 000 RPY= mm Y P R Y P R
17 4.1 g mm Al Al Al Al CDH OBC OBC MLI
18 P Y R OBC2 4.2 Y P R OBC G 1.8G Hz 10Hz MSC.MARC H-A Al Al 4.6 Al 4.4 MS F MS = σ F 4.4 Al R Y P a 18
19 σ a E f t f = 2 1 ν d = MPa 4.2 E f 72.4GPa 0.33t f 1mmd 3.2mm Al 20.0MPa a Al 7 a 16 t f t Ec E c f σ = a = MPa 2 9 h d 1 ν t f 1mmh 450mmt c 18mmd 3.2mmE c 69.6GPaE f 72.4GPa 0.33 Al 20.0MPa a Al Hz 35Hz GPa Al 268.9GPa MPa MPa Hz 22.4Hz
20 T g T g 3µ = I θ 3 P I Y R = Nm km/sR 6378km 1071km rad1degI P I Y T SP T SP = ( 1 + q) = P A L cos i S S S 6 Nm 4.5 P S N/m A S 1.24mL S 0. 25m q 0.6 i 0 deg T m T m = M D 3 r = Nm 4.6 D 1000polecm M emur cm T a T a 1 2 = ρcd AV l 2 = Nm kg/m 3 C d 2.5 A 1.17m 2 V 7315m/sl 0.25m H H = T a ( T + T + T ) + g SP m = Nms VECTRONIC Aerospace Nms SERVO Dual Array Single Head Earth Sensor Assembly 17 SSTL 2-AXIS Sun Sensor 18 Watson Industries ARS-E332-3A 19 SSTL 3-axis Fluxgate Magnetometer
21 rpm 9.36rpm 4.8 T torquer = 10 7 M D 3 r = Nm D 5000polecmM emur cm 1 H max t a = = 743 sec 4.10 T torquer 1Nms Nm 0.02 Nms 1 g 1800 W 4 rpm 5000 mm nT g W mm
22 4.8 Am 2 5 g 750 W 0.5 mm C&DH C&DH Command and Data Handling subsystem SEUSingle Event Upset TDETotal Dose Effect SEU CPU JAXA/ISAS INDEX 20 TDE 64bitMPU OBCOn Board Computer 64bitMPU kg bit = 360 bps 35 sec ( bps HK 7 HK HK 69 69byte CCSDS 1CADU 196byte 1VCDU 0.25Hz 2048 bit 0.25 Hz= 512 bps bps sec= 79 Mbit Mbit = 17.3 kbps sec HK kbps kbps= 18 kbps kbps 22
23 4.9 PA AA SD C&DH kbps Mbyte79Mbit Hz 1.24Mbyte 11.24Mbyte sec Hz byte30mbyte Hz 4 70Hz 100Hz bit 19ch100Hz 12bit HK 2ch bit 19 ch 100 Hz 450 sec + 12 bit 2 ch = 9.91Mbit = 1.24 Mbyte 4.4 HK Mbit = 290 kbps sec 23
24 m 4.10 HK MHzHK 2250MHz C&DH 0.5kbpsHK 20kbps 300kbps HK 5dBi 50g Mono-horn Glegorian m 18 MHz W dbi 46.5 EIRPdBW 6484 MHz dbi 48 K 200 G/TdB 25 24
25 4.11 mm g 650 MHz MHz W 2 % 20 W mm 3 75 g 50 dbi 5 deg mm 25mm 35mm mm g 1 dbi C/N 0 C/N 0 1dB HK C/N 0 dbhz C / N 0 = PE LPS Ld LF LA L L + G / T RA V P E dbw EIRP 100W 0.4W 1dB 5deg 5deg 0deg 5deg 58.6deg 120deg ±60deg 3dB 3dB L PS 0dB L d 3331kmL F - L F =0dB L A 5deg L A =0.3dB L RA 10GHz 0dB L V 0dB G/T 1dB 3dB 300K 313K 300K C/N 0 dbhz C N 0 + L ( E N ) = Lm + b 0 d + BR req G C 4.19 L m 5dB E b /N 0 req 10.5dB 25
26 9.6dB G C 3dB L d dB 2.5dB BR C&DH C/N 0 C/N HK dBHK 23.3dB 11.5dB MHz C/N C/N 0 C/N kg 2W DC-DC SANYO
27 4.14 HK MHz m EIRPdBW dbw db dbi db db db km db db db db G/TdB/K dbi db db dbk K K K C/N 0 dbhz PSK/PM PSK/PM PSK/PM E b /N 0 db db db dbhz db C/N 0 dbhz db
28 C&DH OBC W 4.16 s s W/m deg UR18650F V 3.7 Ah 2.5 mm g
29 47.0g m BAT 800 m BAT = 47.0 ( 4 13) = 2444 g g S BAT VBUS + Vdown S BAT = = = VBAT 3.7 V BUS 12VV BAT V V down V PA BAT Pe Te + Pm T P m PABAT = CtVBUSCd n Pe Te Pm Tm Pd Td X e X e X d P = W 4.23 = Td = P e P d P e WP m W T e WT e 2093/3600 P m / /3600 T m 50.9WT m 800/3600 T d 800/ C t 2.5AhV BUS 12V 800/3600 X e C d X d 0.1n mm 4.18 % 17.0 V 0.52 mg/cm 2 31 %/
30 1 1 P cell P cell ηeff = S E max s cos λ T 100 c ( T 25) W 4.24 S m 2 eff 17.0E s W/m W/m W/m 2 0deg 11.6degT c % T max W W V a V 4 20 ( 3.7 4) 1.2 = V V = 4.25 a S cell Va S cell = = = Vcell 0.52 V cell V PA cell 251 PA cell = = mg/cm 2 m cell 31 mcell = ( 35 8) ( 4 4) = g m w 0.2g ( 35 8) 0.2 = 56 g mw = g
31 E s 1309W/m W/m W/m 2 E e W/m 2 E a a E s E a = ae s 4.30 a OBC 17 5 MLI / /+140 0/+40-15/+50 C&DH OBC 0/+50-30/+55-50/+80-30/+60-20/+70-50/+80-20/
32 = OBC 1/ OBC MLI RTV Al sand blasted
33 Y Y X Z X Z MLI 4.8 Al sand blasted Y
34 2 n i m c i = Q i pi dt dt n i C j= 0 ij n 4 4 ( T T ) R σ ( T T ) i j j= 0 ij i j 4.31 m i i kgc pi i Ws/kgKT i T j ij K Q i i WC ij ij W/KR ij ij m W/m 2 K 4 i Q i Qi = α i Es Ai µ i + ε i Ee Ai Fei ε E A Fa + P i a i i i i i E s W/m 2 A i i m 2 i i =/A i i i E e W/m 2 Fe i i E a W/m 2 Fa i i P i i W Fe i T.C.Bannister Fa i T.C.Bannister 7 ij C ij ka C ij = 4.33 L k W/mKA ij m 2 L ij m Al 177W/mK W/mK 8 ij R ij R ij = ε ε F A 4.34 i j ij i i j ij F ij i j A i i m dt m 2 2.0W Y X X Z Z X X Z Z Y /
35 EM EM EM EM PFM EM PFM PFM H-A BIRD
36 2006 MSC.Nastran MSC.Patran pp H-A JISC DANHER MOTION ndex.php?product_cat_id=87 10 Silicon Designs, Inc Michael Papadopoulos and Ephrahim Garcia, Sensor Placement Methodologies for Dynamic Testing, AIAA Journal, Vol. 36, No. 2, pp , Misawa M. and Kurotaki Y., Sensor Placement for Modal Identification Using Sign Patterns of Target Modes, Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, AIAA paper , ETS- JAXA-RR NAL TM VECTRONIC Aerospace action_wheel.html 17 SERVO 18 SSTL 19 Watson Industries /ARS-E332-xA/ARS-E332-3A_spec.pdf/ 20 Institute of Space and Astronautical Science
37 umion_2.html satellitenentwurf_selfstudy_online/pdf/kap3 _KSE_Thermalhaushalt_www.pdf 25 Frank P. Incropera, and David P. Dewitt, Fundamentals of Heat and Mass Transfer Fifth Edition, John Wiley & Sons,
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50cm 2500mm 300mm 15 CCD 15 100 1 2 3 4 23 SORA Kwak SeungJo 1 1.1 1995 20 2015 6 18 1931 1 2 3 2 ˆ 300mm 2500mm ˆ 2 1.2 WASP 1: 15 2048 2048 CCD 200mm 70 13 WASP 8 1.3 50cm 1 1: CCD 2: 1.4 MOST MOST 15
64 3 g=9.85 m/s 2 g=9.791 m/s 2 36, km ( ) 1 () 2 () m/s : : a) b) kg/m kg/m k
63 3 Section 3.1 g 3.1 3.1: : 64 3 g=9.85 m/s 2 g=9.791 m/s 2 36, km ( ) 1 () 2 () 3 9.8 m/s 2 3.2 3.2: : a) b) 5 15 4 1 1. 1 3 14. 1 3 kg/m 3 2 3.3 1 3 5.8 1 3 kg/m 3 3 2.65 1 3 kg/m 3 4 6 m 3.1. 65 5
1. 4cm 16 cm 4cm 20cm 18 cm L λ(x)=ax [kg/m] A x 4cm A 4cm 12 cm h h Y 0 a G 0.38h a b x r(x) x y = 1 h 0.38h G b h X x r(x) 1 S(x) = πr(x) 2 a,b, h,π
![1. 4cm 16 cm 4cm 20cm 18 cm L λ(x)=ax [kg/m] A x 4cm A 4cm 12 cm h h Y 0 a G 0.38h a b x r(x) x y = 1 h 0.38h G b h X x r(x) 1 S(x) = πr(x) 2 a,b, h,π](/thumbs/101/149329485.jpg "1. 4cm 16 cm 4cm 20cm 18 cm L λ(x)=ax [kg/m] A x 4cm A 4cm 12 cm h h Y 0 a G 0.38h a b x r(x) x y = 1 h 0.38h G b h X x r(x) 1 S(x) = πr(x) 2 a,b, h,π")
. 4cm 6 cm 4cm cm 8 cm λ()=a [kg/m] A 4cm A 4cm cm h h Y a G.38h a b () y = h.38h G b h X () S() = π() a,b, h,π V = ρ M = ρv G = M h S() 3 d a,b, h 4 G = 5 h a b a b = 6 ω() s v m θ() m v () θ() ω() dθ()
(1.2) T D = 0 T = D = 30 kn 1.2 (1.4) 2F W = 0 F = W/2 = 300 kn/2 = 150 kn 1.3 (1.9) R = W 1 + W 2 = = 1100 N. (1.9) W 2 b W 1 a = 0
1 1 1.1 1.) T D = T = D = kn 1. 1.4) F W = F = W/ = kn/ = 15 kn 1. 1.9) R = W 1 + W = 6 + 5 = 11 N. 1.9) W b W 1 a = a = W /W 1 )b = 5/6) = 5 cm 1.4 AB AC P 1, P x, y x, y y x 1.4.) P sin 6 + P 1 sin 45
Microsoft Word - 章末問題
1906 R n m 1 = =1 1 R R= 8h ICP s p s HeNeArXe 1 ns 1 1 1 1 1 17 NaCl 1.3 nm 10nm 3s CuAuAg NaCl CaF - - HeNeAr 1.7(b) 2 2 2d = a + a = 2a d = 2a 2 1 1 N = 8 + 6 = 4 8 2 4 4 2a 3 4 π N πr 3 3 4 ρ = = =
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1 20 9 19 2 1 5 1.1........................ 5 1.2............................. 8 2 9 2.1............................. 9 2.2.............................. 10 3 13 3.1.............................. 13 3.2..................................
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I 2009 c 2009 i 0 1 0.0................................... 1 0.1.............................. 3 0.2.............................. 5 1 7 1.1................................. 7 1.2..............................
= hυ = h c λ υ λ (ev) = 1240 λ W=NE = Nhc λ W= N 2 10-16 λ / / Φe = dqe dt J/s Φ = km Φe(λ)v(λ)dλ THBV3_0101JA Qe = Φedt (W s) Q = Φdt lm s Ee = dφe ds E = dφ ds Φ Φ THBV3_0102JA Me = dφe ds M = dφ ds
Gauss Gauss ɛ 0 E ds = Q (1) xy σ (x, y, z) (2) a ρ(x, y, z) = x 2 + y 2 (r, θ, φ) (1) xy A Gauss ɛ 0 E ds = ɛ 0 EA Q = ρa ɛ 0 EA = ρea E = (ρ/ɛ 0 )e
7 -a 7 -a February 4, 2007 1. 2. 3. 4. 1. 2. 3. 1 Gauss Gauss ɛ 0 E ds = Q (1) xy σ (x, y, z) (2) a ρ(x, y, z) = x 2 + y 2 (r, θ, φ) (1) xy A Gauss ɛ 0 E ds = ɛ 0 EA Q = ρa ɛ 0 EA = ρea E = (ρ/ɛ 0 )e z
8 300 mm 2.50 m/s L/s ( ) 1.13 kg/m MPa 240 C 5.00mm 120 kpa ( ) kg/s c p = 1.02kJ/kgK, R = 287J/kgK kPa, 17.0 C 118 C 870m 3 R = 287J
26 1 22 10 1 2 3 4 5 6 30.0 cm 1.59 kg 110kPa, 42.1 C, 18.0m/s 107kPa c p =1.02kJ/kgK 278J/kgK 30.0 C, 250kPa (c p = 1.02kJ/kgK, R = 287J/kgK) 18.0 C m/s 16.9 C 320kPa 270 m/s C c p = 1.02kJ/kgK, R = 292J/kgK
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( ) c a sin b c b c a cos a c b c a tan b a b cos sin a c b c a ccos b csin (4) Ma k Mg a (Gal) g(98gal) (Gal) a max (K-E) kh Zck.85.6. 4 Ma g a k a g k D τ f c + σ tanφ σ 3 3 /A τ f3 S S τ A σ /A σ /A
0 s T (s) /CR () v 2 /v v 2 v = T (jω) = + jωcr (2) = + (ωcr) 2 ω v R=Ω C=F (b) db db( ) v 2 20 log 0 [db] (3) v R v C v 2 (a) ω (b) : v o v o =
![0 s T (s) /CR () v 2 /v v 2 v = T (jω) = + jωcr (2) = + (ωcr) 2 ω v R=Ω C=F (b) db db( ) v 2 20 log 0 [db] (3) v R v C v 2 (a) ω (b) : v o v o =](/thumbs/91/105491855.jpg "0 s T (s) /CR () v 2 /v v 2 v = T (jω) = + jωcr (2) = + (ωcr) 2 ω v R=Ω C=F (b) db db( ) v 2 20 log 0 [db] (3) v R v C v 2 (a) ω (b) : v o v o =")
RC LC RC 5 2 RC 2 2. /sc sl ( ) s = jω j j ω [rad/s] : C L R sc sl R 2.2 T (s) ( T (s) = = /CR ) + scr s + /CR () 0 s T (s) /CR () v 2 /v v 2 v = T (jω) = + jωcr (2) = + (ωcr) 2 ω v R=Ω C=F (b) db db(
[Ver. 0.2] 1 2 3 4 5 6 7 1 1.1 1.2 1.3 1.4 1.5 1 1.1 1 1.2 1. (elasticity) 2. (plasticity) 3. (strength) 4. 5. (toughness) 6. 1 1.2 1. (elasticity) } 1 1.2 2. (plasticity), 1 1.2 3. (strength) a < b F
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MRR Physical Basis( 1.8.4) METEK MRR 1 MRR 1.1 MRR 24GHz FM-CW(frequency module continuous wave) 30 r+ r f+ f 1.2 1 4 MRR 24GHz 1.3 50mW 1 rf- (waveguide) (horn) 60cm ( monostatic radar) (continuous wave)
http://www.ns.kogakuin.ac.jp/~ft13389/lecture/physics1a2b/ pdf I 1 1 1.1 ( ) 1. 30 m µm 2. 20 cm km 3. 10 m 2 cm 2 4. 5 cm 3 km 3 5. 1 6. 1 7. 1 1.2 ( ) 1. 1 m + 10 cm 2. 1 hr + 6400 sec 3. 3.0 10 5 kg
[1.1] r 1 =10e j(ωt+π/4), r 2 =5e j(ωt+π/3), r 3 =3e j(ωt+π/6) ~r = ~r 1 + ~r 2 + ~r 3 = re j(ωt+φ) =(10e π 4 j +5e π 3 j +3e π 6 j )e jωt
![[1.1] r 1 =10e j(ωt+π/4), r 2 =5e j(ωt+π/3), r 3 =3e j(ωt+π/6) ~r = ~r 1 + ~r 2 + ~r 3 = re j(ωt+φ) =(10e π 4 j +5e π 3 j +3e π 6 j )e jωt](/thumbs/101/152334931.jpg "[1.1] r 1 =10e j(ωt+π/4), r 2 =5e j(ωt+π/3), r 3 =3e j(ωt+π/6) ~r = ~r 1 + ~r 2 + ~r 3 = re j(ωt+φ) =(10e π 4 j +5e π 3 j +3e π 6 j )e jωt")
3.4.7 [.] =e j(t+/4), =5e j(t+/3), 3 =3e j(t+/6) ~ = ~ + ~ + ~ 3 = e j(t+φ) =(e 4 j +5e 3 j +3e 6 j )e jt = e jφ e jt cos φ =cos 4 +5cos 3 +3cos 6 =.69 sin φ =sin 4 +5sin 3 +3sin 6 =.9 =.69 +.9 =7.74 [.]
修士論文
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The Structure and Evolution of Stars I. Basic Equations. M r r =4πr2 ρ () P r = GM rρ. r 2 (2) r: M r : P and ρ: G: M r Lagrange r = M r 4πr 2 rho ( ) P = GM r M r 4πr. 4 (2 ) s(ρ, P ) s(ρ, P ) r L r T
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(a) (b) (c) (d) Wunderlich 2.5.1 = = =90 2 1 (hkl) {hkl} [hkl] L tan 2θ = r L nλ = 2dsinθ dhkl ( ) = 1 2 2 2 h k l + + a b c c l=2 l=1 l=0 Polanyi nλ = I sinφ I: B A a 110 B c 110 b b 110 µ a 110
128 3 II S 1, S 2 Φ 1, Φ 2 Φ 1 = { B( r) n( r)}ds S 1 Φ 2 = { B( r) n( r)}ds (3.3) S 2 S S 1 +S 2 { B( r) n( r)}ds = 0 (3.4) S 1, S 2 { B( r) n( r)}ds
127 3 II 3.1 3.1.1 Φ(t) ϕ em = dφ dt (3.1) B( r) Φ = { B( r) n( r)}ds (3.2) S S n( r) Φ 128 3 II S 1, S 2 Φ 1, Φ 2 Φ 1 = { B( r) n( r)}ds S 1 Φ 2 = { B( r) n( r)}ds (3.3) S 2 S S 1 +S 2 { B( r) n( r)}ds
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Report JS0.5 J Simplicity February 4, 2012 1 J Simplicity HOME http://www.jsimplicity.com/ Preface 2 Report 2 Contents I 5 1 6 1.1..................................... 6 1.2 1 1:................ 7 1.3
I 1
I 1 1 1.1 1. 3 m = 3 1 7 µm. cm = 1 4 km 3. 1 m = 1 1 5 cm 4. 5 cm 3 = 5 1 15 km 3 5. 1 = 36 6. 1 = 8.64 1 4 7. 1 = 3.15 1 7 1 =3 1 7 1 3 π 1. 1. 1 m + 1 cm = 1.1 m. 1 hr + 64 sec = 1 4 sec 3. 3. 1 5 kg
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BELLE TOP 12 1 3 2 BELLE 4 2.1 BELLE........................... 4 2.1.1......................... 4 2.1.2 B B........................ 7 2.1.3 B CP............... 8 2.2 BELLE...................... 9 2.3
A 99% MS-Free Presentation
A 99% MS-Free Presentation 2 Galactic Dynamics (Binney & Tremaine 1987, 2008) Dynamics of Galaxies (Bertin 2000) Dynamical Evolution of Globular Clusters (Spitzer 1987) The Gravitational Million-Body Problem
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TOP URL http://amonphys.web.fc.com/ 1 19 3 19.1................... 3 19.............................. 4 19.3............................... 6 19.4.............................. 8 19.5.............................
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4. ϵ(ν, T ) = c 4 u(ν, T ) ϵ(ν, T ) T ν π4 Planck dx = 0 e x 1 15 U(T ) x 3 U(T ) = σt 4 Stefan-Boltzmann σ 2π5 k 4 15c 2 h 3 = W m 2 K 4 5.
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2.,, Mon, 2006, 401, SAGA, JAPAN Dept. of Mechanical Engineering, Saga Univ., JAPAN 4 Mon, 2006, 401, SAGA, JAPAN Dept. of Mechanical Engineering, Saga Univ., JAPAN 5 Mon, 2006, 401, SAGA, JAPAN Dept.
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35 36 1) 120.07m 2 2 1 LDK 2 2 5 2 3.1.1 ab 3.1.1 3.1.2 910 2730 910 4095 1820 3 8 2F 6.5 6.5 650 650 910 3640 910 910 5460 1820 450 1137.5 1820 1820 1137.5 450 910 3640 2957.5 2957.5 2 910 2730 1820 1820
ω 0 m(ẍ + γẋ + ω0x) 2 = ee (2.118) e iωt x = e 1 m ω0 2 E(ω). (2.119) ω2 iωγ Z N P(ω) = χ(ω)e = exzn (2.120) ϵ = ϵ 0 (1 + χ) ϵ(ω) ϵ 0 = 1 +
2.6 2.6.1 ω 0 m(ẍ + γẋ + ω0x) 2 = ee (2.118) e iωt x = e 1 m ω0 2 E(ω). (2.119) ω2 iωγ Z N P(ω) = χ(ω)e = exzn (2.120) ϵ = ϵ 0 (1 + χ) ϵ(ω) ϵ 0 = 1 + Ne2 m j f j ω 2 j ω2 iωγ j (2.121) Z ω ω j γ j f j
ma22-9 u ( v w) = u v w sin θê = v w sin θ u cos φ = = 2.3 ( a b) ( c d) = ( a c)( b d) ( a d)( b c) ( a b) ( c d) = (a 2 b 3 a 3 b 2 )(c 2 d 3 c 3 d
A 2. x F (t) =f sin ωt x(0) = ẋ(0) = 0 ω θ sin θ θ 3! θ3 v = f mω cos ωt x = f mω (t sin ωt) ω t 0 = f ( cos ωt) mω x ma2-2 t ω x f (t mω ω (ωt ) 6 (ωt)3 = f 6m ωt3 2.2 u ( v w) = v ( w u) = w ( u v) ma22-9
(e ) (µ ) (τ ) ( (ν e,e ) e- (ν µ,µ ) µ- (ν τ,τ ) τ- ) ( ) ( ) ( ) (SU(2) ) (W +,Z 0,W ) * 1) [ ] [ ] [ ] ν e ν µ ν τ e µ τ, e R,µ R,τ R (2.1a
![(e ) (µ ) (τ ) ( (ν e,e ) e- (ν µ,µ ) µ- (ν τ,τ ) τ- ) ( ) ( ) ( ) (SU(2) ) (W +,Z 0,W ) * 1) [ ] [ ] [ ] ν e ν µ ν τ e µ τ, e R,µ R,τ R (2.1a](/thumbs/100/144882653.jpg "(e ) (µ ) (τ ) ( (ν e,e ) e- (ν µ,µ ) µ- (ν τ,τ ) τ- ) ( ) ( ) ( ) (SU(2) ) (W +,Z 0,W ) * 1) [ ] [ ] [ ] ν e ν µ ν τ e µ τ, e R,µ R,τ R (2.1a")
1 2 2.1 (e ) (µ ) (τ ) ( (ν e,e ) e- (ν µ,µ ) µ- (ν τ,τ ) τ- ) ( ) ( ) ( ) (SU(2) ) (W +,Z 0,W ) * 1) [ ] [ ] [ ] ν e ν µ ν τ e µ τ, e R,µ R,τ R (2.1a) L ( ) ) * 2) W Z 1/2 ( - ) d u + e + ν e 1 1 0 0