# Example 12.1 FPS() BEGIN t = 0 s v = 3 ft / s^3 * t^2 + 2 ft / s^2 * t x = 1 ft / s^3 * t^3 + 1 ft / s^2 * t^2 a = 6 ft / s^3 * t + 2 ft / s^2 END func(t,3 s) # Example 12.2 MKS() t = 4 s v = 1 m/s c = -0.4 s / m^2 a = c * v^3 v0 = 60 m/s vv = 1 / sqrt(1 / v0^2 + -2 * c * t) ss = -1 / c * (sqrt(1 / v0^2 - 2 * c * t) - 1 / v0) # Example 12.3 MKS() t = 0 s va = 75 m/s ac = -grav() sa = 40 m vb = 0 m/s sb = sa - (va^2 - vb^2) / (2 * ac) sc = 0 vc = sqrt(vb^2 + 2 * ac * (sc - sb)) # Example 12.4 MKS() s0 = 100 mm s1 = 200 mm v = 2 / s^2 * sqrt(s1^2 - s0^2) # Example 12.5 MKS() BEGIN t = 1 s v = 3 m / s^3 * t^2 - 6 m / s^2 * t ss = 1 m/s^3 * t^3 - 3 m / s^2 * t^2 END s1 = func(t , 0 s) s2 = func(t , 2 s) s3 = func(t , 3.5 s) st = (4 + 4 + 6.125) m dels = 6.125 - 0 vave = dels / 3.5 s # Example 12.9 FPS() t = 2 s x = 8 ft / s * t y = x^2 / 10 ft r = sqrt(x^2 + y^2) vx = 8 ft/s vy = 2 * x * vx / 10 ft v = sqrt(vx^2 + vy^2) qv = atan2(vy,vx); deg ax = 0 ay = 2 * vx^2 / 10 ft a = sqrt(ax^2 + ay^2) qa = atan2(ay,ax); deg # Example 12.10 MKS(deg) t = 0.75 r = [0.5 * sin(2 * t), 0.5 * cos(2 * t), -0.2 * t] m mag(r) ur = r / mag(r) alp = acos(ur[1]) bet = acos(ur[2]) gam = acos(ur[3]) v = [cos(2 * t), -sin(2 * t), -0.2 ] m/s mag(v) a = [-2 * sin(2 * t), -2 * cos(2 * t), 0 ] m/s^2 mag(a) # Example 12.11 MKS(deg) y = -6 m t = sqrt(2 * y / (-grav())) v0 = 12 m/s r = v0 * t # Example 12.12 FPS(deg) v0 = 25 ft/s q = 30 deg v0x = v0 * cos(q) v0y = v0 * sin(q) t = 20 ft / v0x ya = v0y * t - 0.5 * grav() * t^2 # Example 12.13 MKS(deg) sb = -1 m sa = 0 m q = 30 deg t = 1.5 s BEGIN va = 1 m/s e = sa + va * t * sin(q) - 0.5 * grav() * t^2 - sb END solve(e, va) r = va * cos(q) * t BEGIN h = 0 m e = va^2 * sin(q)^2 - 2 * grav() * (h - 1 m) END solve(e,h) # Example 12.14 MKS(deg) v0 = 6 m/s a = 2 m/s^2 x = 1 / 10 m y = x^2 / 20 m vx = x / 10 m q = 45 deg va = 6 rho = (abs(1 + va^2))^1/5 / abs(0.1) # Example 12.15 FPS(deg) at = 7 ft/s^2 r = 300 ft BEGIN t = 1 s v = at * t an = v^2 / r a = sqrt(at^2 + an^2) e = a - 8 ft /s^2 END solve(e,t) # Example 12.16 MKS(deg) c = (0.2 m/s^2) / (1 s) # calibrate t = 1 s a = c * t v = (c / 2) * t^2 ss = (c / 6) * t^3 sb = (3 + 2 * pi() * 2 / 4) m t = (sb * 6 / c)^(1/3) a = c * t v = (c / 2) * t^2 r = 2 m an = v^2 / r aa = sqrt(a^2 + an^2) # Example 12.18 MKS( mm, mm/s, mm/s^2) cq = (1 rad) / (1 s)^3 # calibrate cr = (100 mm) / (1 s)^2 # calibrate t = 1 s q = cq * t^3 qdot = 3 * cq * t^2 qdotdot = 6 * cq * t r = cr * t^2 rdot = 2 * cr * t rdotdot = 2 * cr v = [rdot, r * qdot] mag(v) PolarAngle(v); deg a = [rdotdot - r * qdot^2, r * qdotdot + 2 * rdot * qdot] mag(a) PolarAngle(a); deg # Example 12.19 MKS( ) c = 100 m q = 45 deg qdot = 4 rad /s qdotdot = 0 rad /s^2 r = c / cos(q) rdot = c / cos(q) * tan(q) * qdot rdotdot = c / cos(q) * tan(q)^2 * qdot^2 + c / (cos(q))^3 * qdot^2 v = [rdot, r * qdot] mag(v) PolarAngle(v); deg a = [rdotdot - r * qdot^2, r * qdotdot + 2 * rdot * qdot] mag(a) PolarAngle(a); deg # Example 12.20 FPS c = 0.5 ft v0 = 4 ft/s a0 = 30 ft/s^2 q = 180 deg BEGIN qdot= 4 rad/s qdotdot = 0 rad/s^2 r = c * (1 - cos(q)) rdot = c * sin(q) * qdot rdotdot = c * cos(q) * qdot^2 + c * sin(q) * qdotdot v = [rdot, r * qdot] mag(v) PolarAngle(v); deg a = [rdotdot - r * qdot^2, r * qdotdot + 2 * rdot * qdot] mag(a) PolarAngle(a); deg err1 = mag(a) - a0 err2 = mag(v) - v0 END solve(err1,err2, qdot, qdotdot) # Example 12.21 FPS vb = -6 ft/s va = -3 * vb # Example 12.22 FPS vb = -6 ft/s va = -4 * vb # Example 12.23 MKS va = 2 m/s vb = -va / 4 # Example 12.24 MKS(m, mm/s, mm/s^2) BEGIN x = 1 m y = sqrt(225 m^2 + x^2) - 15 m err = y - 10 m END solve(err, x) vs = 0.5 * 20 (m^2 / s) / sqrt(225 m^2 + x^2) va = 0.5 m/s a = 225 m^2 * va^2 / (225 m^2 + x^2)^1.5 # Example 12.25 MKS(mph, deg) q = 45 deg va = 45 mph * [ cos(q), sin(q)] vt[1] = 60 mph vta = vt - va mag(vta) PolarAngle(vta) # Example 12.26 MKS(kph, km/hr^2, deg) vb = 600 kph va = 700 kph vba = vb - va r = 400 km ab0 = vb^2 / r ab = [ab0, -100 km/hr^2] aa[2] = 50 km/hr^2 aba = ab - aa mag(aba) PolarAngle(aba) # Example 12.27 MKS(deg) vb[2] = -10 m/s q = 60 deg va = -18 m/s * [cos(q), sin(q)] vba = vb - va mag(vba) PolarAngle(vba) r = 100 m abn0 = (12 m/s)^2 / r ab = [-abn0, -3 m/s^2] aa = 2 m/s^2 * [cos(q), sin(q)] aba = ab - aa mag(aba) PolarAngle(aba) # Homework Problems: TBD