Aircraft Load Alleviation and Mode Stabilization (LAMS) Flight Demonstration Test Analysis

Abstract

The Load Alleviation and Mode Stabilization (LAMS) program was conducted to demonstrate the capabilities of an advanced flight control system to alleviate gust loads and control structural modes on a large flexible aircraft using existing aerodynamic control surfaces as force producers.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1969
Accession Number
AD0865310

Entities

People

  • M. A. Bender
  • P. M. Burris

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Actuators
  • Air Force Facilities
  • Aircrafts
  • Airframes
  • Analog Computers
  • Atmospheric Motion
  • Control Surfaces
  • Displacement
  • Dynamic Response
  • Governments
  • Hydraulic Actuators
  • Mach Number
  • Measurement
  • Performance Tests
  • Recording Systems
  • Resonant Frequency
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aquatic Ecology
  • Systems Analysis and Design