150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
1964 state of the art navigation, guidance and control
A boundary value formulation for space vehicle guidance
A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model
Acoustically-Aware Motion Planning with Nonlinear Stochastic MPC
Acoustically-Aware Vehicles: Control Driven Noise Reduction for Urban Air Mobility
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
Active Dihedral Control System for a Torisionally Flexible Wing
Active Dihedral Control System for a Torsionally Flexible Wing
Active external store flutter suppression in the YF-17 flutter model
Active Flow Control (AFC) on the Simplified High-Lift CRM: Lessons Learned
Active flutter suppression using eigenspace and linear quadratic design techniques
Active heat rejection system on Mars Exploration Rover - design changes from Mars Pathfinder
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Adaptive Flight Control for Aircraft Safety Enhancements
Adaptive Optimization for System Performance: Parameterized Differential Dynamic Programming
A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoring
A design method for an optimal attitude regulator for a spinning space station
Advanced Control and Autonomy Research
Advanced control systems for launch vehicles.
Advanced Control Technology and its Potential for Future Transport Aircraft
Advanced detection, isolation, and accommodation of sensor failures - Real-time evaluation
Advanced Technologies for Artificial Intelligence in Flight Applications
Advances in Aircraft System Identification at NASA Langley Research Center
Advancing Electric Propulsion Aircraft Evaluation for Urban Air Mobility: Insights from NASA-Ames
Advantages of multipoint control for vibration testing of complete Ranger flight spacecraft
A dynamic programing analysis of multiple guidance corrections of a trajectory.
Aerodynamic braking trajectories for mars orbit attainment.
Aerodynamic characteristics of a slot-lip aileron and slotted flap for dive brakes
AERODYNAMIC CHARACTERISTICS OF FOUR-DUCT TANDEM VTOL-AIRCRAFT CONFIGURATIONS