This document discusses how to determine the optimal descent path for an airplane. It presents three problems:
1. Deriving a cubic polynomial equation to model the descent path based on conditions of starting altitude, touchdown point, and constant horizontal speed.
2. Showing that the vertical acceleration must be below a maximum value based on the horizontal speed and distance from touchdown.
3. Calculating the distance from the airport at which descent should begin, given constraints on maximum vertical acceleration, starting altitude, and airspeed.
The document solves each problem, derives the relevant equations, and provides an example graph of a descent path satisfying the given conditions.