The most recent Errata is available as a PostScript file Errata.2ed.ps . and as a PDF file Errata.2ed.pdf .

(If you find a typo that is not listed, please let Prof. Prussing know.)

Material covered in the course is in Chapters 1–3 and 5–11 of the text plus other parts as time permits.

Analysis of orbits in an inverse-square gravitational field; elementary rocket dynamics, impulsive orbit transfer and rendezvous, and Lambert's Theorem with applications; patched-conic trajectories, planetary gravity-assist maneuvers, and linearized orbit theory with application to simplified analytical models; perturbations. Prerequisite: AE 202, or consent of instructor. 3 undergraduate hours. 3 or 4 graduate hours.

The n-body problem in an inverse-square gravitational field

The two-body problem; justification, geometry, and dynamics

Time vs. position in orbit: Kepler's equation, universal variables

Orbital elements and related topics

Lambert's theorem with application to spacecraft targeting

Rocket dynamics; the rocket equation and staging

Impulsive orbit transfer and rendezvous; Hohmann, bi-elliptic, and other transfers

Continuous-thrust transfers

Patched-conic techniques and planetary gravity-assist maneuvers

Linear orbit theory; the Hill-Clohessy-Wiltshire (CW) equations

Perturbations due to disturbing accelerations (drag, oblateness, other bodies)