Optimal Control of Active Recoil Mechanisms
Abstract
A servo-valve feedback system with variable control law is proposed for modification of a conventional hydropneumatic recoil mechanism to minimize peak recoil force for any round fired. Phase-plane-delta method of digital simulation is used to simulate the recoil mechanism model. An objective function with direct physical interpretations is developed and non-linear optimization techniques are used to design feedback gains for each firing round. The method is applied to M37 recoil mechanism and significant improvement in recoil force trajectories is obtained.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1977
- Accession Number
- ADA042090
Entities
People
- A. N. Madiwale
- S. M. Wu
Organizations
- University of Wisconsin–Madison