CM: Calculus of Variations Airplane problem

Click For Summary
SUMMARY

The discussion centers on a calculus of variations problem involving an aircraft's flight path from town O to town P, focusing on minimizing flight time in the presence of wind shear. The key equations include the Euler-Lagrange equation and the formulation of flight time as an integral, specifically T = Integral[ ds/(v-wind)] from 0 to D. Participants discuss deriving the plane's ground speed in terms of airspeed (vo), wind speed (V), and the heading angle (phi), as well as approximating the integrand for flight time. The conversation highlights the need for clarity in setting up the integral for optimal path determination.

PREREQUISITES
  • Understanding of calculus of variations
  • Familiarity with the Euler-Lagrange equation
  • Basic knowledge of vector components in physics
  • Experience with integral calculus and optimization techniques
NEXT STEPS
  • Study the derivation of the Euler-Lagrange equation in detail
  • Learn how to set up and solve integrals in Mathematica
  • Explore optimization techniques in calculus of variations
  • Investigate applications of wind shear in flight dynamics
USEFUL FOR

Students and professionals in aerospace engineering, mathematicians specializing in optimization, and anyone involved in flight path analysis and calculus of variations.

Hazerboy
Messages
15
Reaction score
0

Homework Statement


"An aircraft whose airspeed is vo has to tfly from town O (at the origin) to town P, which is a distance D due east. There is a steady gentle wind shear, such that v-wind = Vy(x-hat) [the wind shear is in the x direction...]. x and y are measured east and north respectively. Find the path, y = y(x), which the plane should follow to minimize its flight time.

Part a): find the plane's grounds peed in terms of vo, V, and phi (the angle by which the plane head sto the north of east), and the plane's position

b): write down the time of flight as an integral of the form Integral[ f(x), x, {0, D}] (for those of you familiar with mathematica I used their wacky notation... basically its just an integral of f(x)dx from 0-> D). Show that if we assume that y' and phi both remain small then the integrand f takes the approximate form: f = (1+ 1/2 * y'^2 ) / (1+ ky) where k = V/v0

the remaining two parts involve finding y(x) though I need help on this part first.

Homework Equations



The euler-lagrange equation

The Attempt at a Solution



This is a problem in calculus of variations, so basically what we're doing here is optimizing the Time integral.

for part a), i said that V-plane = Vx *(x-hat) + Vy*(y-hat) (we don't need to worry about the altitude here). Vx = vo * cos( phi ) + Vy where Vy is the wind shear

Vy = vo * sin(phi)

for part b) here's what I don't understand here... t = distance/velocity, , so shouldn't T = Integral[ ds/v-wind] from 0 -> D, where ds = (dx^2 + dy^2)^1/2? I don't understand how I'm supposed to find the shortest time using only dx, or f(x) * dx... Can someone please explain this to me? The problem tells what what f(x) should be given the approximation but I'm unsure of how to set it up... the problem set is due wednesday morning.

I feel like I can adequately use the Euler - lagrange equation once i figure this part out and set it up.

Thanks!

-Trent
 
Last edited:
Physics news on Phys.org
*bump
 

Similar threads

Replies
2
Views
2K
  • · Replies 12 ·
Replies
12
Views
3K
  • · Replies 22 ·
Replies
22
Views
2K
  • · Replies 13 ·
Replies
13
Views
1K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 10 ·
Replies
10
Views
3K
  • · Replies 8 ·
Replies
8
Views
8K
  • · Replies 3 ·
Replies
3
Views
1K
  • · Replies 33 ·
2
Replies
33
Views
5K
  • · Replies 4 ·
Replies
4
Views
2K