Simulation of LV missile steering
Abstract
A computerized simulation of missile kinematic trajectories from fixed launchers was carried out using a continuous system modelling program. The study includes a description of kinematic analysis of missile steering and steering strategies for moving targets. The results are presented in form of diagrams and tables, showing the applications of the simulation method.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- July 1979
- Bibcode:
- 1979STIN...8018085O
- Keywords:
-
- Command And Control;
- Computerized Simulation;
- Missile Control;
- Missile Trajectories;
- Impact Prediction;
- Kinematics;
- Launch Vehicles and Space Vehicles