Supersonic Trajectory Optimization for Minimum-Fuel Flights in Three Dimensions
PPE Attitude Profile Reference for the Earth Orbit Raising Phase
The NASA Langley Challenge on Optimization Under Uncertainty
Strategies for Uncertainty Modeling and Optimization Under Uncertainty
Peak-Seeking Optimization of Trim for Reduced Fuel Consumption: Flight-Test Results
Peak-Seeking Optimization of Trim for Reduced Fuel Consumption: Flight-Test Results
Optimized Algorithms for Prediction Within Robotic Tele-Operative Interfaces
Impact of Slot Substitution on CTOP Performance
A manual optimal guidance scheme using a predictive model.
Process Product Integrity Audits: A Hardware Auditing Technique for the '90s'
Optimal guidance for ascent trajectories into circular orbits.
Optimal Control Strategies for Imaging Using Formation Flying Spacecraft
Optimal and suboptimal guidance and control for low thrust orbital transfer.
A direct and analytical solution for space flight guidance functions.
Research in optimization and guidance theory
Optimization of hydraulic thrust vector control systems for launch vehicles, volume III, section 2
Peak-Seeking Optimization of Trim for Reduced Fuel Consumption: Flight-Test Results
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance for a low thrust interplanetary vehicle.
Optimization of Flight Control of Spacecraft
Near Real-Time Closed-Loop Optimal Control Feedback for Spacecraft Attitude Maneuvers
Interactive Aircraft Flight Control and Aeroelastic Stabilization
The Application of Optimal Control Technqiues to Advanced Manned Missions, Volume 1
Control-System Techniques for Improved Departure/Spin Resistance for Fighter Aircraft
Optimal Control in Ordiny Dy$)Mys Systems
Quasilinearization determination of optimum finite-thrust orbital transfers.
Preliminary Design Study of a Lateral-Directional Control System Using Thrust Vectoring
Optimization problems caused by interaction of guidance and propellant systems.
Optimization problems caused by interaction of guidance and propellant systems.
Rapid determination of near-optimum linear pitch programs for rocket boosters.
Cut-off insensitive guidance with variable time of flight
Practical Scheme for Adaptive Aircraft Flight Control Systems
Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design
Solar Sail Roadmap Mission GN and C Challenges
Investigation of Abort Procedures for Space Shuttle-Type Vehicles
Trajectory Optimization for Spacecraft Collision Avoidance
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design