Analysis of Unmanned, Tethered, Rotary-Wing Platforms (Vol. 1 or 2)

Abstract

A study was conducted (1) to determine the feasibility of an unmanned, tethered, rotary-wing vehicle as an elevated platform for target detection sensors or other payloads and (2) to determine the best approach to implementing specified design and performance requirements. A review was made of current and past developments of tethered platforms, and a large number of rotary-wing lift concepts, rotor drive and long-endurance power concepts, and stabilization and control concepts were formulated for evaluation. Mathematical models were designed and a digital computer was used to generate quantitative data on air vehicle size, weight, horsepower, etc., for alternative systems. A turboshaft-driven synchropter, utilizing fuel pumped from the ground for long endurance, was recommended as the best overall approach for an unmanned tethered platform. The synchropter, with cyclic pitch controls, will provide a stable platform for mission sensors and can be operated, without attention from the ground, by a simple automatic flight control system.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1974
Accession Number
AD0785581

Entities

People

  • Arvid Plaks
  • Lawrence H. Mcneill
  • William E. Blackburn

Organizations

  • Kaman Corporation

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Calorific Value
  • Control Systems
  • Detection
  • Detectors
  • Flight Control Systems
  • Fuel Systems
  • Gas Turbines
  • Ground Control Stations
  • Helicopters
  • Internal Combustion Engines
  • Rotary Wing Aircraft
  • Turbines
  • Turboshaft Engines

Fields of Study

  • Engineering

Readers

  • Aerial Unmanned Vehicle Swarm Micro Periodontal Dentistry.
  • Aerospace Engineering
  • Systems Analysis and Design

Technology Areas

  • Autonomy