I & q = M 2 m && z = F z
m & z = F I & q = 2 M
1/26
Fr=0.00.6 λ/lm 0.53.0 a 2.0 cm
1
2
3
4
5
6
UUV UUV 7
No Yes 形 成 音 場 の 計 算 想 定 さ れ る 画 像 8
9
PE PE FDTD 10 x(m) y(m) x(m) y(m) PE
FDTD FDTD t t t 11
FDTD x(m) y(m) FDTD 12 x(m)
x(m) y(m) x(m) x(m) 13
FDTD 0.59 1 1.34 1 14
FDTD FDTD 16 Hz9.4cm 15
x(m) y(m) x(m) y(m) x(m) y(m) x(m) y(m) FDTD z(m) y(m) 16
x(m) y(m) x(m) y(m) x(m) y(m) x(m) y(m) z(m) y(m) FDTD 17
FDTD FD FDTD 18
Defense Technology Symposium 2011
-12-11 -10-9 -8-7 -6-5 -4-3 -2-1 X +1 +2 +3 +4 +5 +6 Defense Technology Symposium 2011
LBDd 10316.48.74.5 22 3 ( Defense Technology Symposium 2011
Defense Technology Symposium 2011
10/10 15 35 15 3 L WL Defense Technology Symposium 2011
1.6m 30 Defense Technology Symposium 2011 1.5
2002MSC137(76) 1st,2nd overshoot angle δ Ψ (deg.) δ δ δ Ψ 2nd overshoot angle 0 Ψ (s) 1 st overshoot angle Defense Technology Symposium 2011
1 st overshoot angle (deg.) 25 10/10 20 15 10 5 B A C A B C 0 L WL /V (sec) Defense Technology Symposium 2011
作 業 時 の 操 艦 性 Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
-12-11 -10-9 -8-7 -6-5 -4-3 -2-1 X +1 +2 +3 +4 +5 +6 Defense Technology Symposium 2011
DDH
OQQ: OQQ
Fire Control
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/
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Defense Technology Symposium 2011
LBDd 6010.14.52.5 570 ton 24 3 Defense Technology Symposium 2011 * GlassFiber Reinforced Plastic
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011
Defense Technology Symposium 2011 1
LBDd 849.110.38.5m 2,950 ton 21 3 Defense Technology Symposium 2011 2
CG Defense Technology Symposium 2011 3
Defense Technology Symposium 2011 4
Defense Technology Symposium 2011 5
Defense Technology Symposium 2011 6
Defense Technology Symposium 2011 7
Defense Technology Symposium 2011 8
m Defense Technology Symposium 2011 9
Defense Technology Symposium 2011 10
15 30 0 0 Defense Technology Symposium 2011 11
Defense Technology Symposium 2011 12
UAV
H23-25
IED
STANAG 4569level4 STANAG NATO
370mm 600mm 1100mm
LCV :
/
g/cm 3 (MPa) PECS2 B 4 C1 2.81 472 3340Hv NS3 B 4 C 2.41 395 3023Hv PECS2 Al 2 O 3 4 3.98 556 2110Hv NS3
g/cm 3 (MPa) PECS A SiC 3.23 719 2490Hv PECS SiC 3.17 705 2460Hv 3.10 400 2200
92 92
架 設 速 度 ( 公 称 )
A B C A B C C A B
v10
1
2
3
4
5
6
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小 型 高 出 力 半 導 体 レー ザによる 小 型 発 振 器 S/A 8
9
10
11
u u u u u u u u
u u
u u
2
3
4
M&Sの階層 システム統合レベル シミュレーションの目的 大規模空間でネットワークにより 連携した将来装備システム SoS: System of Systems の コンセプト検討等 シミュレーション統合システム 統合防空システムシミュレーション システムレベル コンポーネントレベル 装備システム構築のための設計支 援及び試験評価 開発官 研究所 サブシステム 構成要素の設計及 び試験評価 研究所 5
6
シ ミ ュ レ ー シ ョ ン シ ミ ュ レ ー シ ョ ン 7
8
9
10
( 6 分 類 3 0 種 類 ) ( 1 9 5 モ デ ル ) 11
12
13
14
15
16
2
3
NCW: Network Centric Warfare, SoS : System of Systems
7
8
9
10
11
12
2
3
4
5
6
7
8
9
10
11
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13
2011 Voice Analysis Reveals Soldier s Beat (Prosodic Features of Speech for Estimating Mental and Physical Stress)
Verbal Vocal Visual Mehrabian, A. (1971). Silent messages. Wadsworth, Belmont, California.
米 国 国 防 総 省 PSE CVSA Lantern Vericator LVA 米 ソ ( 宇 宙 ) NASA NATO 1965-1975 - 1985-1995 - 2005 - NASA S40 S50 S60 H 7 H17 航 空 事 故 調 査 で 利 用 5 1969
2009.. Hiroto Kikuchi (2010). Effects of Mental Stressors during Flight on Prosodic Features of Speech and Autonomic Nervous Responses. Annual Seminar of the International Society of Air Safety Investigators. 20113 Lacerda
http://www.baic.jp/cinemri/atr-baic_3.gif
20091 15 1530 USAirways #1549(A320) NY La Guardia NC Charlotte
15:28.50 teterboro 15:28.34 15:28.11 15:29.03 teterboro 15:29.25 15:29.28 15:27.46 220 15:27.36 CTS-1539, E/G 15:26.04 CTS-1549, 15,000 15:25.51 CTS-1549, 700ft, 5,000ft http://www.nytimes.com/interactive/2009/01/15/nyregion/20090115-plane-crash-970.html
5 km http://en.wikipedia.org/wiki/file:us_airways_flight_1549.svg
CTS-1549, 700ft, 5,000ft High 1.2 CTS-1549, 15,000 CTS-1539,E/G teterboro teterboro 220 4 1.1 200 3 2 1 1.0 0.9 0.8 0.7 150 100 50 0 0.6 15: 25:00 26:00 27:00 28:00 29:00 30:00 FAA (http://www.faa.gov/data_research/accident_incident/1549/) 0
2011 Voice Analysis Reveals Soldier s Beat (Prosodic Features of Speech for Estimating Mental and Physical Stress)
Personal Protective Ensemble http://nsrdec.natick.army.mil/media/fact/individual/ap-ppe.pdf
[ CH PIB 2 C(CH 3 ) 2 ] n 500,000 SiO 2 SiO 2 12nm [ CF 2 CF 2 ] n 1 µm C CNT 2nm 15µm
http://www.daca.com/productsdaca/mcpage.html http://www.internationalcrystal.net/icl77a.htm# µ
g t h http://japan.mt.com/jp/ja/home/products/laboratory_ Weighing_Solutions/MX-UMX/XP26.html
D = πθ 16 2 h 2 M t / M 1.2 M t /M 1 t 1/2 0.8 0.8 θ 0.6 0.6 0.4 0.4 θ 0.2 0.2 0 0 40 80 120 0 0 200 400 600 800 1000 t Time 1/2 (s 1/2 ) s 1/2
D (10-9 cm 2 /s) 150 100 50 PIB PIB + SiO2 PIB + PTFE PIB + CNT 10 phr parts per hundred rubber 0
SiC *2 Si GaN GaN 2000 GaAs 2000 1970 *5 InP InP 19 9 0
S(12,12) S(2,2) S(11,11) S(1,1) S 11 m6 m5 S 22 m2 m1 Sweep_CEM1.DC_CEM1.DC.IC_CES2.i, A Sweep_CEM1.DC_CEM1.DC.IC_CEM1.i, A 1.1 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0 freq (100.0MHz to 10.00GHz) -0.1 0 5 10 15 20 25 30 35 40 45 50 VCE_CEM
3
4
p p p 5
#1 #2 6
180 180 0 ε f 0
8
300mm 1 10GHz #1 θ: θ=6#1 300mm 9
RCS30 10GHz #2 θ: θ=30#2 10
RCS [dbsm] 1 01 ] [ RCS10GHz 300MHz RCS 01 20dB 11 [db] 0-5 -10-15 -20-25 -30-35 300MHz 8 9 10 11 12 [GHz]
RCS [dbsm] 30 15-50 ] [ RCS 10GHz 12 500MHz RCS RCS+30 20dB [db] 0-10 -20-30 -40-60 500MHz 8 9 10 11 12 [GHz]
13
14
1
2
22 RCS : RadarCrossSection R max = PG t (4π ) 2 2 λ 3 RCS S min 1/ 4 Pt : G : λ : S min : RCS Radar Cross Section 1/10(10dB) 1/100(20dB) 1/1000(30dB) 0.56 0.32 0.18 3
RCS RCS RCS
Gihon Evaluation Scattering System ( matlab) RCS PO RCS POEEC MOM( )MLFMM 5
x z y z z x y x y RCS RCS 0180[deg.] RCS 6
X z x + - α y z [deg.] α 0 -α [ rad] x y RCS RCS 7
10 10[m] 5[m] ( ) 150[m] 20[m] 28.3[m] 1[m] 10[m] 8
Z=0 9
10 z x + y 10[deg.] : -32-31[dBsm] 10
x z y z x y 1m 11
10[GHz] x + z y : -18-17 [dbsm] 1m z x + y [m] RCS 4.97[dBsm] : 45[dBsm ] RCS 12
RCS RCS RCS RCS RCS RCS 13