Cooperative control of regenerative braking and hydraulic braking of an electrified passenger car
Design of impact angle control guidance laws via high-performance sliding mode control
Strategies to minimize the fuel consumption of passenger cars during car-following scenarios
Effect of geometric parameters on the spray cone angle in the pressure swirl injector
Model predictive regenerative braking control for lightweight electric vehicles with in-wheel motors
Robust autopilot design of uncertain bank-to-turn missiles using state-space disturbance observers
Estimation of effective compression ratio for engines utilizing flexible intake valve actuation
An approach to optimization of airport taxiway scheduling and traversal under uncertainty
Estimation models for the preliminary design of electromechanical actuators
Comparison of regenerative braking technologies for heavy goods vehicles in urban environments
Parametric effects in a scramjet engine on the interaction between the air stream and the injection
Consensus-based reconfigurable controller design for unmanned aerial vehicle formation flight
Multi-objective optimization of a composite wing subject to strength and aeroelastic constraints
Evaluation of the efficiency and the drive cycle emissions for a hydrogen direct-injection engine
Extended state observer-based robust pitch autopilot design for tactical missiles
The control strategy of optimal brake energy recovery for a parallel hydraulic hybrid vehicle
Effect of the air-conditioning system on the fuel economy in a gasoline engine vehicle
Motion control of an electromagnetic valve actuator based on the inverse system method
Automated conflict resolution, arrival management, and weather avoidance for air traffic management
Optimal trajectory planning for path convergence in three-dimensional space
Identification of a non-linear F/A-18 model by the use of fuzzy logic and neural network methods
Low-thrust trajectory design as a constrained global optimization problem
Neural network-based sliding mode variable structure control for Mars entry