Flight testing of the AIM/RIM-7M missile, preflight analysis
Abstract
The AIM/RIM-7M missile is the most recent version of the AIM-7 missile series. It is in the preproduction phase and has completed most of the preproduction flight test evaluation. A description is presented of the preflight simulation techniques used, taking into account the value of the techniques in predicting the results of actual flights. The AIM/RIM-7M is a semiactive, radar-guided homing missile with sophisticated onboard digital processing. It may be launched from either an aircraft or a surface system. To a large degree, the AIM/RIM-7M represents problems typical of all guided missiles. The described techniques are directly applicable to radar-guided missiles and generically to all types of guided missiles. Attention is given to simulation bay activities, the anechoic chamber, aspects of RF control, the target array, computer models, aspects of preflight simulations, and the test setup.
- Publication:
-
AIAA
- Pub Date:
- November 1981
- Bibcode:
- 1981flte.confQ....H
- Keywords:
-
- Airborne/Spaceborne Computers;
- Avionics;
- Flight Simulation;
- Flight Tests;
- Missile Tests;
- Preflight Analysis;
- Anechoic Chambers;
- Computerized Simulation;
- Homing Devices;
- Missile Control;
- Missile Tracking;
- Radar Tracking;
- Launch Vehicles and Space Vehicles