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Theory of Helicopter Damping in Pitch or Roll and a Comparison With Flight Measurements
Terminal Control, Time-Lags and Dynamic Programming
On Control of Linear Systems with Time Lags
Application of Analytical Techniques to Flight Evaluations in Critical Control Areas
Effects of Aeroelasticity on the Stability and Control Characteristics of Airplanes
Project Suric - Phase V - Volume I
The Experience Curves. Vol. II. 85% Through 99%
Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles-II
Flexible Flight Vehicle Transfer Function Factors for Use in Autopilot Preliminary Design
Research on Satellite Attitude Control Using Plasma Pinch Engines
Science and Competition of Two Systems Cybernetics, New Stage
Prediction of Trajectory of Space Vehicle under Discrete Control
Long-Range Planning and Technological Forecasting: An Annotated Bibliography, Supplement I
Work Year 1966 Rac-Army Work Program. 1 Sep 1965-31 Aug 1966
Research on Satellite Attitude Control Using Plasma Pinch Engines
System Effects on Propellant Storability and Vehicle Performance
The Calculation of Automatic Control Systems
Optimal Control in Ordiny Dy$)Mys Systems
Bionics Symposium 1966, Held in Dayton, Ohio On 3-5 May 1966. Short Paper Pre-Prints
Synthesis of Flight Control Systems Subject to Vehicle Parameter Variations
Use of the Landing Point Designator to Land the Lunar Module to a Given Target - Project APOLLO
Optimal Guidance and Control in a Missile Defense System
Regional Principles for the Functional Classification of Rural Roads and Urban Streets
Analysis of the Uadps Icp Procurement Decision Rules and the Cares Program for Inventory Management
Stationkeeping a 24-Hr Satellite Using Solar Radiation Pressure
Analysis and Design of Space Vehicle Flight Control Systems. Volume VI - Stochastic Effects
Filtering for Stochastic Processes with Applications to Guidance
Minimum Sensitivity Design of Attitude Control Systems Final Report
Optimization of Three-Dimensional Reentry Trajectories
The Reliability of a Space Vehicle Launcher System - a Theoretical Approach
Trajectory Optimization by Method of Steepest Descent. Volume II. User'S Manual
Derivation of the Optimal Control for an All-Weather Airplane Landing System
A Study of Optimal Evasive Maneuvers Against Air to Air Missiles
Short Course on Guidance and Control for Aerospace Vehicles
Fixed Wing Stability and Control: Theory and Flight Test Techniques
Economics of Sounding Rocket Utilization