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100-kHz Coherent Raman Thermometry in a Free-Piston Shock Tube
Mitigating Time-Delay in Nonlinear Dynamics Inversion for Multirotor Unmanned Aerial Vehicles
Effects of Copper Foam Wall/Obstacles on the Deflagration-to-Detonation Transition
Interaction Behavior of Pulsejet Engines
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles
Effects of Propellant Slosh on Touchdown Stability for Landing Vehicles
Optimal Midcourse Guidance for Dual-Pulse Rocket Using Pseudospectral Sequential Convex Programming
Aerodynamic Stabilization of a Finless Projectile with Active Nose Deflection
Active Valve Resonant Pulse Combustor for Pressure Gain Combustion Applications
Adaptive State-Dependent Riccati Equation Control for Formation Reconfiguration in Cislunar Space
Event-Triggered Antidisturbance Control Design for Aeroengine Systems via Switched Models
Wall Heat Loads in a Cryogenic Rocket Thrust Chamber During Thermoacoustic Instabilities
Unexpected Collision Detection, Estimation, and Reaction for a Free-Flying Orbital Robot
Acoustic Modes in a Plenum Downstream of a Multitube Pulse Detonation Combustor
Dynamic Features of Internal and External Flowfields of Pulsejet Engines
Minimum-Eigenvalue-Based Fault-Tolerant Adaptive Dynamic Control for Spacecraft
Collision-Inclusive Trajectory Optimization for Free-Flying Spacecraft
Flow Characterization of Heavy-Lift Helicopter Rear Fuselage with Pulsed Jets for Separation Control
Gas Thermometry by Optical Emission Spectroscopy Enhanced with Probing Nanosecond Plasma Pulse
Frequency and Spark Timing Effects on Thrust for Pulse Detonation Engine
to Mars: A Combined Robotic/Piloted Mars Mission
Integrated Optimization for Single-Stage-to-Orbit Using a Pulse Detonation Engine
Direct Thrust Measurement of an Electron Cyclotron Resonance Plasma Thruster
Low-Cost Laser Range-Measurement-Based Terrain-Following Concept and Error Analysis
Real-Time Closed-Loop System Identification of a Quadcopter
Time-Resolved Flowfield Measurements of Momentum-Driven Pulsed Transient Jets
Coherent Structures in the Actively Controlled Wake of a High-Lift Configuration
Coupled Microvibration Analysis of Space Optical Load Platform
Satellite Formation-Containment Flying Control with Collision Avoidance
Simulations and Flight Tests of a New Nonlinear Controller for the EAGLE Lander
Acoustic Characterization of Pulse Detonation Combustors
Utilization of Nonthermal Plasma in Pulse Detonation Engine Ignition
Effect of Ionic Liquid Composition on Colloid Thruster Emission and Thrust Performance
Non-Premixed Burner-Attached Jet Flames in Crossflow Pulsed at Resonance Frequency
Quaternion-Based Bang-Bang Attitude Stabilizer for Rotating Rigid Bodies
Emulating Scaled Clohessy–Wiltshire Dynamics on an Air-Bearing Spacecraft Simulation Testbed
Validation of Pulse-Detonation Operation in Low-Ambient-Pressure Environment
Theoretical Model for the Gust Performance of Closed-Loop Flight Control
Experimental Study of Pressure Gain Combustion with Hypergolic Rocket Propellants
Thrust Characteristics of High-Density Helicon Plasma Using Argon and Xenon Gases