Cantilever Beam Design for Projectile Internal Moving Mass Systems

Author:

Rogers Jonathan1,Costello Mark21

Affiliation:

1. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30318

2. Mem. ASME

Abstract

Internal masses that undergo controlled translation within a projectile have been shown to be effective control mechanisms for smart weapons. However, internal mass oscillation must occur at the projectile roll frequency to generate sufficient control force. This can lead to high power requirements and place a heavy burden on designers attempting to allocate volume within the projectile for internal mass actuators and power supplies. The work reported here outlines a conceptual design for an internal translating mass system using a cantilever beam and electromagnetic actuators. The cantilever beam acts as the moving mass, vibrating at the projectile roll frequency to generate control force. First, a dynamic model is developed to describe the system. Then the natural frequency, damping ratio, and length of the beam are varied to study their affects on force required and total battery size. Trade studies also examine the effect on force required and total battery size of a roll-rate feedback system that actively changes beam elastic properties. Results show that, with proper sizing and specifications, the cantilever beam control mechanism requires relatively small batteries and low actuator control forces with minimum actuator complexity and space requirements.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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2. Internal Moving Mass Actuator Control for Mars Entry Guidance;Journal of Spacecraft and Rockets;2015-09

3. Computational Improvements to Multibody Projectile Dynamics Simulation;AIAA Modeling and Simulation Technologies Conference;2014-06-13

4. Flight Dynamic Simulation for Multibody Aircraft Configurations;Journal of Guidance, Control, and Dynamics;2012-11

5. Rate regulation of a suborbital reentry payload by moving-mass actuators;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-01-06

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