Deriving Gauss' Variational Equation for True Anomaly

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SUMMARY

The discussion focuses on deriving Gauss' Variational differential equation for the true anomaly, f, with respect to time. Key components include the position vector expressed in terms of unit vectors \hat r, \hat \theta, and \hat h, as well as the perturbative acceleration. The participants emphasize the importance of correctly substituting the radius and velocity components to simplify the equation. The final expression to derive is p cos(f) * (term1 + term2), where term1 and term2 must be shown to sum to one.

PREREQUISITES
  • Understanding of orbital mechanics and true anomaly
  • Familiarity with vector components in polar coordinates (\hat r, \hat \theta, \hat h)
  • Knowledge of perturbation theory in celestial mechanics
  • Ability to manipulate trigonometric identities and algebraic expressions
NEXT STEPS
  • Study the derivation of Gauss' Variational equations in detail
  • Learn about perturbative acceleration in orbital dynamics
  • Explore the application of trigonometric identities in simplifying equations
  • Review the concepts of angular momentum and its role in orbital mechanics
USEFUL FOR

Students and researchers in celestial mechanics, particularly those working on orbital dynamics and variational equations. This discussion is beneficial for anyone looking to deepen their understanding of true anomaly and its mathematical derivation.

jsandberg
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Homework Statement


Derive the Gauss Variational differential equation for the true anomaly, f, with respect to time using components along the radius, angular velocity, and a unit vector orthogonal to those two (ir,itheta,ih).


Homework Equations


Sorry, I don't know how to use Latex. But I have attached the equations I need to start from and get to! ad is the perturbation, r_underline is the position vector, r is the norm of the position vector, v is the velocity vetor, h is the angular momentum, f is the tru anomaly, e is the eccentricity, p is the semilatus rectum.

The Attempt at a Solution


See attached handwritten solution- the first two lines are given in the assignment. I just can't seem to get the equation simplifed to the final equation.

View attachment df_dt.zip

View attachment Derivation df_dt.pdf
 
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Your mistake is right at the start. Unfortunately this means everything you did was wrong.

Your mistake was in expressing the position and velocity vectors in terms of \hat x, \hat y, and \hat z. You should have expressed these in the same coordinate system in which the perturbative acceleration is expressed -- in other words, \hat r, \hat \theta, and \hat h. The position vector is simply \mathbf r = r \hat r. I'll leave velocity up to you.

Hint: It does not take two pages of math to derive the result.
 


Thank you for your quick response! Yes, changing the radius and velocity components helped a lot. I am still having trouble simplifyin the equation, however (see attached).

Thanks again for your time.
 

Attachments



What's wrong? The last expression is exactly what you want to derive. Is your problem going from the penultimate expression to the last one? In other words, you are having a problem with showing

\left(1+\frac r p\right)re(1-\sin^2 f) + \frac{r^2} p \cos f = p\cos f

Hint: All you need are 1-\sin^2 f = \cos^2 f and r=p/(1+e\cos f).
 


Yes, that is where my problem is. Do I substitute the equation for "r" every time I see an "r"?
 


This is homework. I've given a couple of hints. I'll give one more: Factor p\cos f out of each term on the left hand side. In other words, rewrite the left hand side as p cos(f) * (term1 + term2). Now show that term1+term2 is identically one.
 


Thanks for all your help! Much appreciated.
 

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