3.2.23 · D5Orbital Mechanics & Astrodynamics

Question bank — Combined maneuvers — optimal split between plane change and velocity change

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Figure — Combined maneuvers — optimal split between plane change and velocity change
Figure — Combined maneuvers — optimal split between plane change and velocity change

True or false — justify

Combining a speed change and a plane change into one angled burn is never worse than doing them separately.
True. By the triangle inequality the third side can never exceed the two-leg path ; they are equal only in degenerate cases (e.g. ).
A plane change at orbital speed costs less than of delta-v.
False. The equal-speed cost is exactly — you spend your whole orbital speed again just to turn.
Doubling the plane-change angle roughly doubles the plane-change cost.
False for small angles and false in general — cost goes as , not . For tiny angles so it is roughly linear, but for large angles the sine flattens and eventually the cost saturates.
At (flipping the orbit completely) the plane change costs .
True. — you must kill your entire velocity and rebuild it in the opposite sense, the most expensive turn possible.
For a fixed total inclination change , splitting it 50/50 between the two Hohmann burns minimizes fuel.
False. What must be equal is the marginal cost per extra degree, not the degrees themselves. Since the burns run at very different speeds, the optimal split of is lopsided — most of ends up at the slow burn.
If both burns happen at the same orbital speed, the optimal split is symmetric.
True. When , the balance condition becomes ; with equal speed products the two functions have identical shape, so the equation is satisfied when , i.e. .
Raising apoapsis just to do a plane change out there always saves fuel.
False. You pay extra to raise and re-lower apoapsis. It only wins when the plane-change angle is large enough that the savings on beat the raise/lower cost — the logic behind Bi-elliptic Transfer.
The combined-maneuver formula reduces to the pure plane-change formula when .
True. Setting gives via the half-angle identity.
The optimal plane-change split depends on the shape of the transfer orbit, not just the endpoint speeds.
True. The speeds that enter the condition come from the Vis-viva Equation evaluated on the actual transfer ellipse, so a different transfer (e.g. Bi-elliptic Transfer) shifts where the plane change wants to live.

Spot the error

"I'll do the whole plane change at periapsis so I get it over with while thrusting hard." — find the flaw.
Periapsis is where is largest, and turning cost scales with . Doing all the turn there () is the single most expensive choice; the turn belongs at apoapsis where is smallest.
"Since for a speed change, the combined burn is just that plus the plane change: ." — find the flaw.
That formula adds two separate burns (walking two sides of the velocity triangle) and overcounts. The single combined burn is the triangle's third side , which is the sum by the triangle inequality.
"The optimal split condition sets the two 's equal: ." — find the flaw.
No — it sets the two derivatives equal in magnitude (marginal costs), i.e. . The total burns themselves are usually quite unequal.
", so at the cost is ." — find the flaw.
At , , giving , not . The cross term does not vanish — it is maximal.
"A plane change is free if I do it exactly at apoapsis." — find the flaw.
Apoapsis has the smallest speed, not zero speed. The cost shrinks with but is never zero for a real orbit ( always).
"Because appears, the plane-change angle must be under for the formula to work." — find the flaw.
is defined for every angle; the formula holds for all from to . Beyond , simply goes negative, making the term add to the cost.

Why questions

Why do we set the two derivatives and equal to find the best split?
The total cost is minimized where its derivative vanishes: . Since raising raises burn 1 but lowers burn 2, this says the marginal cost of one more degree of turn must be equal at both burns — if it weren't, you'd shift a degree to the cheaper burn and save, so you can't already be at the minimum.
Why does the plane change migrate to the slower burn rather than the faster one?
Differentiate one burn's cost: only carries , so . The marginal cost of a degree of turn is thus proportional to the local speed products . The slow (apoapsis) burn has tiny products, so its marginal cost stays low until it has absorbed most of the turn.
Why is the law of cosines — and not, say, the Pythagorean theorem — the right tool for combined ?
Pythagoras needs a right angle between and ; here the included angle is arbitrary (look at the velocity triangle above). The Law of Cosines generalizes Pythagoras to any included angle, which is exactly the velocity-triangle situation.
Why does appear (half the angle) instead of in the pure plane-change cost?
The equal-speed velocity triangle is isosceles; dropping a perpendicular from the apex bisects both and the base . In the resulting right half-triangle , giving — the half-angle identity made geometric.
Why is a plane change so much more expensive than an equal-magnitude speed change?
A speed change costs only — the difference of speeds. A plane change costs , which is scaled by the full speed ; you must redirect the entire velocity vector sideways.
Why does combining beat separating even though the single burn "does more work"?
Delta-v measures vector magnitude, not tasks. Two separate burns trace two sides of the velocity triangle; the combined burn is the direct third side, and a straight path is never longer than a detour (triangle inequality).
Why does the order "speed change then plane change" (or the reverse) not change the separate cost formula ?
Either ordering traces the same two legs of the triangle in opposite order, and addition is commutative — so the total is identical. The factor just fixes the plane change to whichever speed you are moving at when you turn; doing it after speeding up to is why the second leg uses , not .
Why does the optimal split depend on the actual transfer speeds and not just the inclination ?
The balance condition weights each burn by its speed products ; those come from the Vis-viva Equation on the transfer orbit, so faster/slower endpoints reshuffle where the turn is cheapest.

Edge cases

What is when and ?
Zero — no change in speed or direction means no burn. The formula gives , the sanity floor.
What happens to the optimal split as the two orbits become the same size ()?
The speed products at both burns approach equality, so the equal-marginal-cost condition pushes the split toward symmetric, .
What is the plane-change cost as apoapsis is pushed to infinity (bi-elliptic limit)?
, so the turn cost — asymptotically free out there. But the total is not free: you first pay a raise burn to fling apoapsis outward and a return burn to drop back, and these two burns stay finite (and grow with how far you go), which is why the full Bi-elliptic Transfer delta-v never actually reaches zero.
If the required speed change is zero but a plane change is needed, does "combining" still help?
There is nothing to combine it with at that point, so you pay the pure . The lesson shifts to location: perform it where is smallest, i.e. at apoapsis.
What does the combined formula give when (starting from rest)?
— you simply need to build the full final velocity from scratch; the plane-change angle no longer matters because there is no initial direction to turn from.
At with , is combining better than separating?
They tie. Combined gives ; separating gives . This is the degenerate case where the "triangle" collapses to a straight line and the inequality becomes equality.
Recall One-line self-test before you leave

Where does a plane change belong, and into how many burns should it fold with a speed change? Answer ::: At the slowest point of the orbit (apoapsis), folded into a single angled burn — "turn where slow, burn in one throw."