3.4.1 · D1Rocket Flight Mechanics

Foundations — Coordinate systems — Earth-Centered Inertial (ECI), Earth-Centered Earth-Fixed (ECEF), North-East-Down (NED), launch, bo

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Before you can read a single formula in the parent note, you need to own every symbol it throws at you. We build them one at a time, each earning its place before the next arrives.


0. What is an "arrow" and what is a "frame"?

Figure — Coordinate systems — Earth-Centered Inertial (ECI), Earth-Centered Earth-Fixed (ECEF), North-East-Down (NED), launch, bo

1. Components and coordinates —


2. Unit vectors —


3. Right-handed axes — why the order X, Y, Z is not free

Figure — Coordinate systems — Earth-Centered Inertial (ECI), Earth-Centered Earth-Fixed (ECEF), North-East-Down (NED), launch, bo

4. The angle symbols —

Angles say how much one thing is turned from another. Each Greek letter has a fixed job:

Figure — Coordinate systems — Earth-Centered Inertial (ECI), Earth-Centered Earth-Fixed (ECEF), North-East-Down (NED), launch, bo

5. Sine and cosine — turning an angle into two numbers

This is why Example 2 in the parent note says "with , ": the cosine of a right angle is zero.


6. The dot product — "how much of A lies along B"


7. The cross product — building a perpendicular direction

Figure — Coordinate systems — Earth-Centered Inertial (ECI), Earth-Centered Earth-Fixed (ECEF), North-East-Down (NED), launch, bo

8. The rotation matrix — the machine that swaps rulers


9. Rate of rotation and time


How it all feeds the topic

Vector arrow r

Components rx ry rz

Unit vectors x hat Z hat r hat

Dot product

Cross product

Right handed axes

Angles phi lambda theta

Sine and cosine

Rotation matrix R

East velocity omega x r

Frame transforms ECI ECEF NED body

Rate omega and time t

Coordinate systems topic 3.4.1

See the parent map here: parent topic.


Where each foundation is used next

  • Dot & cross products, right-handedness → building the NED rulers and the transport theorem: Rotating Reference Frames and Coriolis Force.
  • Rotation matrix , , → the rotation chain: Rotation Matrices and Euler Angles, and the alternative in Quaternions for Attitude.
  • Inertial vs non-inertial frames → why we integrate in ECI: Newton's Laws and Inertial Frames.
  • Latitude → the launch bonus and inclination: Launch Azimuth and Orbital Inclination, and the fine print in Geodetic vs Geocentric Latitude.
  • The full equations these frames carryRocket Equations of Motion.

Equipment checklist

Recall Self-test: can you answer each before reading the parent note?

What does the hat in mean? ::: A vector of length exactly 1 — a pure direction, here pointing straight out from Earth's centre. What does a rotation matrix do to an arrow's components? ::: Re-reads the same physical arrow against a rotated set of rulers, giving a new column of three numbers. Why is ? ::: Because a rotation is orthonormal (), so undoing it is just transposing the table. Which product gives "how much of A lies along B"? ::: The dot product, . Which product builds a new direction perpendicular to two others? ::: The cross product, , direction by the right-hand rule. What is on the unit circle? ::: The horizontal shadow of a length-1 arrow swept through angle . What does represent? ::: The angle Earth has spun through after time — the sole difference between ECI and ECEF. Latitude vs longitude — which is ? ::: is latitude (North–South, flat rungs); is longitude (East–West, orange-slice lines). Why must axes be right-handed? ::: So the third axis (from the cross product) has the correct sign — otherwise East comes out as West.