2-Way Driven Compressor for Hybrid Vehicle Climate Control System
6-DOF Synchronization Control for Multiple Spacecraft Formation Flying
93-3776 Design of a Flight Control System for a Highly Maneuverable Aircraft Using Synthesis
93-3785 Cut-Off Insensitive Guidance with Variable Time of Flight
93-3790 Reentry Control to a Drag vs. Energy Profile
93-3808 Integrated Flight/Propulsion Control: Subsystem Specifications for Performance
93-3810 TVC Control for the AIAA Design Challenge Airplane
93-3822 On Navigation of a Robotic Land Vehicle
93-3846 Optimal Performance of Airplanes Flying through Windshear
93-3849 Helicopter Flight Control Law Design with and without Rotor-State Feedback
93-3851 Benefits of Variable Rotor Speed in Integrated Helicopter/Engine Control
93-3852 Automated Control of Aircraft in Formation Flight
93-3881 A New Technique for Nonlinear Control of Aircraft
93-3890 Spacecraft Intercept Guidance Using Zero Effort Miss Steering
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 35, Class 1, Grade 190, Fiber 1
350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 35, Class 1, Grade 190, Fiber 2