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Free-Flight Dynamics of an Aeroshell/Drogue Parachute System
Free-Flight Dynamics of an Aeroshell/Drogue Parachute System
Theory of spin filtering in non-magnetic resonant tunneling diodes
Automated model checking with promela/spin
Doppler aided attitude determination for spin stabilized spacecraft
Electron-spin g-factor engineering with Si/Ge heterostructures
An estimate of motion between the spin axis and the hotspots over the past century
Mars Science Laboratory Orbit Determination Data Pre-Processing
Attitude Determination of Spin Stabilized Spacecraft Using a Digital Aspect Sensor
Nutation Control During Precession of a Spin-Stabilized Spacecraft
Techniques for Earth-Pointing Attitude Control of a Spacecraft
Techniques for Earth-Pointing Attitude Control of a Spacecraft
Pendulum-Type Nutation Damper Used in the NASA Atmospheric Structure Satellite, S-6
Guidance and Control of a Man-Portable Precision Munition Concept
Attitude determination of spin stabilized spacecraft using a digital aspect sensor
Hovering Dual-Spin Vehicle Groundwork for Bias Momentum Sizing Validation Experiment
SIMULATOR STUDIES OF SIMPLE ATTITUDE CONTROL FOR SPIN-STABILIZED VEHICLES
Using SPIN model checking for verification of flight software
Using SPIN model checking for flight software verification
Effect of Inertia Properties on Attitude Stability of Nonrigid Spin-Stabilized Spacecraft
A viscous ring damper for a freely precessing satellite.
Free-Spinning Characteristics of a 1/30-Scale Model of the Grumman WF-2 Airplane
Some design considerations for spin-stabilized satellites with rigid expandable structures
Scanning celestial attitude determination system /SCADS/.
Spinning satellite attitude control via the Earth's magnetic field.
Motion of a spinning satellite during the deployment of asymmetrical appendages.
Design and evaluation study of deployable solar array for spinning satellites Final report
MINIGUIDE - A SIMPLIFIED ATTITUDE CONTROL FOR SPINSTABILIZED VEHICLES
Passive Stabilization of Rotating Spacecraft Using Dynamic Fluid-Pressure Equilibrium
Motion of a spinning satellite during the deployment of n asymmetrical appendages.
Design and Evaluation Study of Deployable Solar Array for Spinning Satellites Final Report
Advanced Technological Satellite Electro-Mechanical Despun Antenna Final Report
A Manual Abort Guidance Technique with Concentric Flight Plan Rendezvous
Passive Stabilization of Rotating Spacecraft Using Dynamic Fluid-Pressure Equilibrium
Pendulum-type nutation damper used in the nasa atmospheric structure satellite, s-6