150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
A brief review of aircraft controls research opportunities in the general aviation field
A centralized optimal controller for formation flying spacecraft
Achieving control and interoperability through unified model-based systems and software engineering
A comparative analysis of loop heat pipe based thermal architectures for spacecraft thermal control
A comparison of theory and experiment for aeroelastic stability of a hingeless rotor model in hover
Activation and initial test operations of large rocket engine - Turbopump test facilities.
Active control landing gear for ground loads alleviation
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
Active control of gust- and interference-induced vibration of tilt-rotor aircraft
Active control of wing rock of a delta wing at post-stall using tangential leading edge blowing
Active controls technology to maximize structural efficiency