Solving For Unknown Vector Components

Click For Summary
SUMMARY

The discussion focuses on calculating the original aircraft speed (Pi) prior to wind impact, given the final speed (Pf), wind speed, and direction. The aircraft's initial heading is 241° with a speed of 683 f/s, while the wind travels south at 32 f/s. The equations derived include vector components for both the aircraft and wind, leading to the conclusion that Pi can be calculated using the formula Pi^2 = (Pf - W*cosβ)^2 + (W*sinβ)^2. The final calculated value for Pi is approximately 649 f/s.

PREREQUISITES
  • Understanding of vector components in physics
  • Familiarity with trigonometric functions and their applications
  • Knowledge of coordinate systems for vector analysis
  • Ability to solve quadratic equations
NEXT STEPS
  • Study vector addition and subtraction in physics
  • Learn about resolving vectors into components
  • Explore the application of trigonometric identities in physics problems
  • Investigate the effects of wind on aircraft navigation and speed calculations
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in navigation and flight dynamics will benefit from this discussion, particularly those interested in vector analysis and aircraft performance under varying wind conditions.

Badmachine
Messages
13
Reaction score
0

Homework Statement



Is it possible to determine aircraft speed prior to contact with noted wind, if resulting aircraft speed, original aircraft heading, wind speed and wind direction and final aircraft heading are known?

Homework Equations



P (plane): Bearing 241° (traveling approximately southwest) @ "X" f/s.
W (wind): Traveling south @ 32 f/s.

Plane and wind components represented by ordered pairs:

P = ["X" f/s cos(241°), "X" f/s sin(241°)] = ?, ?
W = [-32 f/s cos(90°), -32 f/s sin(90°)] = 0, -32

? + 0 = ?
? + (-32) = ?

||P + W|| = ?² + ?² = ?^(1/2) = 710 f/s

tan −1(?/?) = 62.24° + 180° = 242.24°

Displacement = 242.24° - 241° = 1.24°

The Attempt at a Solution

 
Last edited:
Physics news on Phys.org
Select a co-ordinate axis so that final direction of the plane (Pf) is along -x-axis.
Let the angle of the initial direction of the plane (Pi) with he new x-axis be α.
Let the angle of the direction of the wind (W) with he new x-axis be β. From the given data you can find β.
Now sum of the x-components of Pi and W is equal to Pf.
And y component of Pi is equal and opposite to y-component of W.
Write the equations and solve.
 
Does the solution require eliminating the wind components or inverting the wind compinent's values?
 
Badmachine said:
Does the solution require eliminating the wind components or inverting the wind compinent's values?
The two equations become
(Pi)x + (W)x = (Pf) ...(1)

(Pi)y + (W)y = 0...(2)
Rearrange the equations.

(Pi)x = - (W)x + (Pf) ...(3)

(Pi)y = -(W)y ...(4)
Square eq. 3 and 4 and add to get (Pi)
 
Thanks rl. Let's see if I am following you correctly.

(Pi)x = - (W)x + (Pf)

(Pi)y = -(W)y



(Pi)x = - (0)x + (P[710 f/s]f)

(Pi)y = -(32)y

710² + 32² = 505,124^(1/2) = 710.72

Apparently I'm performing the calculations incorrectly, as Pi = 683 f/s (value omitted in original post).

Original problem:

P (plane): Bearing 241° (traveling approximately southwest) @ 683 f/s (465 mph); W (wind): traveling south @ 32 f/s (22 mph)

[683 f/s cos(241°), 683 f/s sin(241°)] = -331, -597
[-32 f/s cos(90°), -32 f/s sin(90°)] = 0, -32

-331 + 0 = -331
-597 + (-32) = -629

||P + W|| = 331² + 629² = 505, 2021/2 = 710 f/s

tan −1(629/331) = 62.24° + 180° = 242.24°

Displacement = 242.24° - 241° = 1.24°
 
Last edited:
What is required in the original problem?
For example, if the want to cross a river and reach the opposite bank, you have to row in the upstream direction. Similarly which velocity is given in the problem?
 
rl.bhat said:
What is required in the original problem?

To determine the final aircraft velocity (Pf) and angular aircraft displacement from original heading, after application of a given wind.

Had hoped to learn how to "reverse engineer" for the original aircraft speed (Pi) or even heading simply based on other knowns.
 
OK. It can be done in the following way. Refer my post#2 and #4
Pi*cosα + W*cosβ = Pf Or
Pi*cosα = Pf - W*cosβ
Pi*sinα = W*sinβ
Pi^2 = ( Pf - W*cosβ )^2 + (W*sinβ)^2
In the given problem, if the velocity of plane is Pf, then β = 270degrees - 241 degrees.
So using the above equation you can find Pi.
 
Thanks rl.

Perhaps I miscalculated somehwere, but at this stage I arrive at Pi = 649 f/s (as opposed to 683 f/s)

β = 270degrees - 241 degrees = 29
Pi^2 = ( Pf - W*cosβ )^2 + (W*sinβ)^2
Pi^2 = [710 - (-32)*cos29]^2 + [(-32)*sin29)]^2
421,400 = 421,159 + 241
649 f/s
 

Similar threads

  • · Replies 2 ·
Replies
2
Views
3K
Replies
11
Views
2K
Replies
3
Views
1K
  • · Replies 6 ·
Replies
6
Views
2K
  • · Replies 9 ·
Replies
9
Views
2K
  • · Replies 29 ·
Replies
29
Views
3K
  • · Replies 5 ·
Replies
5
Views
2K
Replies
3
Views
3K
  • · Replies 2 ·
Replies
2
Views
2K
  • · Replies 1 ·
Replies
1
Views
1K