SLIDE 1 The Parachute Problem
Ethan Retherford
College of the Redwoods
May 15, 2015
SLIDE 2
Introduction
The “parachute problem” is commonly seen in the beginning of an introductory differential equation course and involves the use of Second or first-order ODEs (ordinary differential equations). The traditional problem to be modeled and analyzed involves a parachutist jumping from an aircraft at a specific height, x0, and falling towards Earth under the influence of gravity.
SLIDE 3
SLIDE 4
SLIDE 5
The Basic Model
We start with analyzing the parachutist’s free-fall from, x0.This is done by applying Newton’s Second Law of Motion, ΣF = ma.
SLIDE 6
Free-fall and parachute deployed stages of the jump
x0 Fg = −mg Fd = −k1v Free − fall x0 Fg = −mg Fd = −k2v Parachute Deployed Assume the parachute deploys instantaneously at td
SLIDE 7 Deriving the differential equations k =
0 ≤ t < td k2, t ≥ td ΣF = ma Fg + Fd = ma −mg − kv = ma
ma + kv = −mg
SLIDE 8
Deriving the differential equations
First-order system for position and velocity x′ = v, x(0) = x0 v ′ = −g − k mv, v(0) = 0.
SLIDE 9 Free-fall During free-fall k = k1 for t < td v ′ + k1 mv = −g, v(0) = 0 Solving for v(t), we get the velocity while in free-fall v(t) = mg k1
SLIDE 10 Free-fall Now, to obtain the position x(t) we can sub v(t) into the position equation x′ = v x′ = mg k1
x(0) = x0 Solving x(t) = x0 − mg k1 t − m2g k2
1
SLIDE 11 Parachute is deployed
v ′ + k2 m v = −g, v(t−
d ) = v(t+ d )
Obtaining the general solution and using the initial condition mg k1
k2 + Ce−k2td/m C = mg k2 ek2td/m + mg k1 ek2td/m e−k1td/m − 1
- Substituting C back into v(t), t ≥ td
v(t) = mg k1 e−k2(t−td)/m e−k1td/m − 1
kd
SLIDE 12 Parachute is deployed
Use Same method for Position x(t) = x0 − mg k1 td −
m2g k2
1
+ m2g k1k2
k2
2
k2 − mgt k2
SLIDE 13 Position and Velocity for Entire Jump
x(t) = x0 − mg
k1 t − m2g k2
1
t < td x0 − mg
k1 td −
k2
1 + m2g
k1k2
k2
2
k2
− mgt
k2 ,
t ≥ td v(t) =
mg k1
t < td
mg k1 e−k2(t−td)/m
e−k1td/m − 1
k2
t ≥ td
SLIDE 14
Acceleration and Terminal Velocity Acceleration a = v ′ = −g − k mv Terminal velocity, when a = 0 vt = −mg k
SLIDE 15 Analysis of Basic Model
k1 = 14 kg/s, k2 = 160 kg/s
Position (x/200) Velocity (v/10) Acceleration (a/g)
10 20 30 40 time (s)
5 10
SLIDE 16
Real-World Considerations
Goals to meet The parachute deployment is not instantaneous and a certain amount of force is experienced during the process. The snatch force is the acceleration at the first instant when the assembly reaches full extension; the opening shock, or jerk, is the shock produced while the parachute deploys. The snatch force felt when the lines are fully elongated is a heavy, but smooth, tug that is not particularly uncomfortable. While this force depends on the weight of the jumper, it should not exceed 500 lbs (≈ 3Gs for a 165 lb (75 kg)person). The landing velocity should be no worse than a free-fall from a 5′ (1.52 m) wall–between 4.6 and 5.2 m/s.
SLIDE 17
Deployment stage Added
x0 Fg = −mg Fd = −k1v Free − fall x0 Fg = −mg Fd = −kdv Deployment x0 Fg = −mg Fd = −k2v Parachute Deployed
SLIDE 18
SLIDE 19
Connecting the constant states in a continuous manner
k(t) = k1, 0 ≤ t < td kd, td ≤ t < td + τd k2, t ≥ td + τd.
SLIDE 20 Linear Interpolation
20 23.5 t 14 160 k(t)
(td, k1) (td+τd, k2)
kd(t) = k1 + k2 − k1 τ (t − td)
SLIDE 21 Plots with Linear Interpolation
Position (x/1000) Velocity (v/10) Acceleration (a/g)
20 40 60 80 100 time (s)
2
SLIDE 22
Jerk
j(t) := da dt = −k′(t) m v(t) − k(t) m a(t)
SLIDE 23 Linear Interpolation with Jerk
Position (x/1000) Velocity (v/10) Acceleration (a/g) Jerk (j/g)
20 22 24 26 time (s)
2 4
SLIDE 24 Cubic Interpolation
20 23.5 t 14 160 k(t)
(td, k1) (td+τd, k2)
kd(t) = (−2k2 + 2k1) t − td τd 3 + (3k2 − 3k1) t − td τd 2 + k1.
SLIDE 25 Plots with Cubic Interpolation
Position (x/1000) Velocity (v/10) Acceleration (a/g) Jerk (j/g)
20 22 24 26 time (s)
2 4