A method for deriving the reference trajectory of a descending flight vehicle
Abstract
A method is proposed for reducing a multicriterial nonsmooth main control problem to a single-criterion smooth problem. The sufficient conditions for solving the terminal guidance problems are determined. A procedure is presented for deriving optimal control using nonlinear programming methods and a specially developed set of applied software.
- Publication:
-
Aviatsionnaia Tekhnika
- Pub Date:
- 1992
- Bibcode:
- 1992AvTek...3...10S
- Keywords:
-
- Descent Trajectories;
- Flight Control;
- Nonlinear Programming;
- Optimal Control;
- Terminal Guidance;
- Trajectory Optimization;
- Computer Programs;
- Flight Vehicles;
- Problem Solving;
- Reference Systems;
- Astrodynamics