航空情報サーキュラー(AIC)発行案について(1/X)
1. A 1-1/2 1 5 (1) sin (x y) = sin x cos y cos x sin y Z = e ix e iy (2) x < 1 x = 0 (i) 1 1 x (ii) log (1 + x) log (3) (i) (ii) 0 1 xe x dx dx (x x x
19
B [ 0.1 ] x > 0 x 6= 1 f(x) µ 1 1 xn 1 + sin sin x 1 x 1 f(x) := lim. n x n (1) lim inf f(x) (2) lim sup f(x) x 1 0 x 1 0 (
11
1. 1 BASIC PC BASIC BASIC BASIC Fortran WS PC (1.3) 1 + x 1 x = x = (1.1) 1 + x = (1.2) 1 + x 1 = (1.
150
1 (utility) 1.1 x u(x) x i x j u(x i ) u(x j ) u (x) 0, u (x) 0 u (x) x u(x) (Marginal Utility) 1.2 Cobb-Daglas 2 x 1, x 2 u(x 1, x 2 ) max x 1,x 2 u(
14
1 1.1 p(x n+1 x n, x n 1, x n 2, ) = p(x n+1 x n ) (x n ) (x n+1 ) * (I Q) 1 ( 1 Q 1 Q n 0(n ) I + Q + Q 2 + = (I Q) ] q q +/. * q
17
B 38 1 (x, y), (x, y, z) (x 1, x 2 ) (x 1, x 2, x 3 ) 2 : x 2 + y 2 = 1. (parameter) x = cos t, y = sin t. y = f(x) r(t) = (x(t), y(t), z(t)), a t b.
38
2015 : x 1 + x 2 = 1 (1) x 2 = 2x x 1 x 2 (x 1, x 2 ) N x y = Ax (2) M y A M N x 1 3
50
x y 1 x 1 y 1 2 x 2 y 2 3 x 3 y 3... x ( ) 2
103
, 1 ( f n (x))dx d dx ( f n (x)) 1 f n (x)dx d dx f n(x) lim f n (x) = [, 1] x f n (x) = n x x 1 f n (x) = x f n (x) = x 1 x n n f n(x) = [, 1] f n (x
19
7. 1 max max min f g h h(x) = max{f(x), g(x)} f g h l(x) l(x) = min{f(x), g(x)} f g 1 f g h(x) = max{f(x), g(x)} l(x) = min{f(x), g(x)} h(x) = 1 (f(x)
29
Trapezoidal Rule θ = 1/ x n x n 1 t = 1 [f(t n 1, x n 1 ) + f(t n, x n )] (6) 1. dx dt = f(t, x), x(t 0) = x 0 (7) t [t 0, t 1 ] f t [t 0, t 1 ], x x
28
2 1/2 1/4 x 1 x 2 x 1, x 2 9 3x 1 + 2x 2 9 (1.1) 1/3 RDA 1 15 x /4 RDA 1 6 x /6 1 x 1 3 x 2 15 x (1.2) (1.3) (1.4) 1 2 (1.5) x 1
22
n Y 1 (x),..., Y n (x) 1 W (Y 1 (x),..., Y n (x)) 0 W (Y 1 (x),..., Y n (x)) = Y 1 (x)... Y n (x) Y 1(x)... Y n(x) (x)... Y n (n 1) (x) Y (n 1)
32
(iii) 0 V, x V, x + 0 = x. 0. (iv) x V, y V, x + y = 0., y x, y = x. (v) 1x = x. (vii) (α + β)x = αx + βx. (viii) (αβ)x = α(βx)., V, C.,,., (1)
21
1 y x y = α + x β+ε (1) x y (2) x y (1) (2) (1) y (2) x y (1) (2) y x y ε x 12 x y 3 3 β x β x 1 1 β 3 1
20
2 1,, x = 1 a i f i = i i a i f i. media ( ): x 1, x 2,..., x,. mode ( ): x 1, x 2,..., x,., ( ). 2., : box plot ( ): x variace ( ): σ 2 = 1 (x k x) 2
47
2 2.1 x x v x a x x (x = 0) x[m] x v x (1s) v x [m/s] = 1 [m]. (1) 1 s velocity v v x x 1 SI 2 [m/s] (1) t[s] (1) t t v x [m/s] = t [m]. (2) t 3
24
Z[i] Z[i] π 4,1 (x) π 4,3 (x) 1 x (x ) 2 log x π m,a (x) 1 x ϕ(m) log x 1.1 ( ). π(x) x (a, m) = 1 π m,a (x) x modm a 1 π m,a (x) 1 ϕ(m) π(x)
18
x T = (x 1,, x M ) x T x M K C 1,, C K 22 x w y 1: 2 2
21
x i [, b], (i 0, 1, 2,, n),, [, b], [, b] [x 0, x 1 ] [x 1, x 2 ] [x n 1, x n ] ( 2 ). x 0 x 1 x 2 x 3 x n 1 x n b 2: [, b].,, (1) x 0, x 1, x 2,, x n
29