Landing and Takeoff Roll-Out Augmentation.

Abstract

The results of a computer study on four roll-out guidance control laws and a nosewheel steering configuration is included herein. Beam convergence, ground speed, and crosswind effects were included in the simulation. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1974
Accession Number
ADA043526

Entities

People

  • Vincent Muehter

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Landings
  • Aircrafts
  • Control Systems
  • Flight Control Systems
  • Ground Speed
  • Guidance
  • Inertial Navigation
  • Landing
  • Landing Gear
  • Navigation
  • New Jersey
  • Nose Wheels
  • Simulations
  • Steady State
  • Surfaces
  • Wind

Readers

  • Aerospace Engineering
  • Aviation Safety and Air Traffic Management
  • Control Systems Engineering.