Observability studies for spacecraft attitude determination based on temperature data
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Y2O3 Based Spray-On Cryogenic Thermal Control Coating Study
Lissajous Orbit Control for the Deep Space Climate Observatory Sun-Earth L1 Libration Point Mission
Global Precipitation Measurement Mission Launch and Commissioning
Resume of hinge-moment data for unshielded horn- balanced control surfaces
Smart Twisting Active Rotor (STAR2): U.S. Update
A technique for optimal final value control of powered flight trajectories.
QUENCHING OF ADAPTIVE CONTROL SYSTEM RESPONSE TO TEST SIGNAL
Magnetic control of satellite attitude.
A design method for an optimal attitude regulator for a spinning space station
FLUID FLIGHT CONTROL SYSTEM ON TAP FOR SATURN
Extensions to the Galileo Attitude Control System for the Probe Mission
Modal method for analysis of free rotations of spacecraft.
Active heat rejection system on Mars Exploration Rover - design changes from Mars Pathfinder
Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 317
Pneumatic system structure for circulation control aircraft
An analysis of a nonlinear instability in the implementation of a VTOL control system during hover
Flutter Tests of Some Simple Models at a Mach Number of 7.2 in Helium Flow
Side-force alleviation on slender, pointed forebodies at high angles of attack
Aeroelastic stability and control of an oblique wing
Systematic Wind-Tunnel Measurements on Missiles
Decoupler pylon: wing/store flutter suppressor
Directional solar absorptance measurements
The application of temperature rate measure- ments to the determination of thermal emittances
Aeroelastic stability and control of an oblique wing - Wind tunnel experiments
Heat Pipes for Space Applications Part 1 - Axially Grooved Heat Pipes
Optimum guidance for a low thrust interplanetary vehicle.
Flow Physics Study of Sweeping Jet Actuation on a NACA 0015 Swept Wing Configuration
Attitude instability regions of a spinning symmetric satellite in an elliptic orbit.
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity