Controllers and Autopilot Modes for RPV Simulation Program.
Abstract
Several sets of conventional roll-pitch-yaw control systems are synthesized for a conventional air-to-ground strike RPV. Linear and bang-bang logics are developed for the inner (rate control) loops. Outer (position control) loops and automatic target homing (guidance) loops are also developed. The control systems are programmed for a digital, real-time simulation (implemented on the AMRL PDP-12 Computer) of the RPV strike phase. The control system simulator is intended for use as a tool to evaluate the effectiveness of control augmentation for manual piloting of an RPV.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1976
- Accession Number
- ADA025792
Entities
People
- Milford R. Derrick