Front wheel speed sensors detect rotational changes to identify wheelies, suppressing engine power while avoiding noise from road vibrations.
A positioning system estimates remote vehicle location using signal characteristics to identify misbehaving nodes.
Iterative engine model updates compare virtual sensor values to actual measurements for precise component quality tracking.
A cabin coolant heater warms fuel cell stacks and vehicle cabins by routing heated coolant through dedicated branches.
Replacing mechanical drives with electric pumps and fans enables predictive control that reduces fuel consumption by preventing coolant overshoots.
LED light assemblies replace halogen lamps in precision approach path indicators, reducing maintenance costs while ensuring reliable runway guidance.
A control method delays oil pump shutdown after engine stop to maintain lubricant flow through turbocharger bearings.
An engine control apparatus adjusts target torque using vehicle speed and accelerator opening data to optimize output delivery.
A control unit nullifies starter failure tests during voltage drops to prevent erroneous eco-run shutdowns.
Profile-view schematics segment flight plans into active legs, reducing display complexity and steep learning curves for flight crews.
Switching between 2-stroke and 4-stroke HCCI modes doubles power output while maintaining high efficiency and minimizing NOx emissions.
Coupling device connects split crankshaft sections within main bearings to maintain compact engine dimensions.
A calculation module determines combustion chamber heater temperature based on effective resistance for precise thermal management.
An indirect integration method computes indicated mean effective pressure using sparse input data and cubic spline interpolation.
A customizable flight tracking display system sequences real-time aviation data and personalized messages for upscale airport operations.
A fusion processor aligns confidence values with azimuth angles to produce fused curves for automated target recognition.
Ground-based devices transmit stored route data wirelessly to vehicles, providing information outside the vehicle sensing range.
Runway slope compensation module adjusts elevator and symmetric wing surface commands to stabilize aircraft descent profiles.
An adaptive engine control system dynamically updates spark timing values to optimize combustion and achieve mean best torque.
A monitoring system processes sensor and GPS data to generate clear utilization reports for field assets.
Infrastructure-based sensing devices and servers collect environmental data to guide autonomous vehicles along calculated routes.
A motor controller adds torque to the engine crankshaft to stabilize power delivery during compression strokes.
Engine start logic triggers when oil contaminants exceed thresholds, reducing friction wear while conserving stored energy.
A hybrid vehicle control system monitors driver presence using brake and shift sensors to manage internal combustion engine startup.
Algorithm distinguishes thermostat failures from vehicle configuration errors by monitoring temperature changes during intrusive fan or thermostat actuation.
A vehicular peer-to-peer apparatus adjusts identifier sets based on traffic information to optimize resource allocation.
A flow rate adjustment method for variable geometry turbochargers uses pre-stored nozzle data to correct actuator positioning errors.
An engine control system reduces idle speed based on wheel slip values to manage torque output.
A FADEC control system predicts turbine temperature changes to mitigate transient spikes.
Merging RNP and precision deviation displays reduces pilot workload during abrupt guidance mode transitions.
An engine control device predicts minimum battery voltage using resistance and current data to enable automatic restarts.
Adjusting ignition timing by comparing measured engine roughness to a threshold limit reduces hydrocarbon emissions during cold starts.
Electronic document validation replaces manual handling to reduce turn-around time during aircraft preparation.
A conditioning circuit processes probe resistance to detect shaft shear conditions in gas turbine engines.
Dual-counter hardware detects toothless parts in engine pulse signals, resolving vibration-induced misjudgment at low speeds.
A fuel quality monitoring system detects impurities and adjusts engine parameters to maintain optimal performance.
Aircraft flight management system merges navigation, terrain, and weather sensors to calculate safe reconfiguration paths around moving objects.
A correction system generates learned values to compensate throttle position for airflow variations.
A travel distance estimating apparatus calculates remaining range using a segmented consumed energy equation incorporating idling, acceleration, and resistance factors.
A fault manager assigns state indicators to mobile platform components and transmits periodic summaries via wireless links.
Autonomous onboard systems predict closest point of approach and integrate compensation commands with control signals, reducing air traffic controller workload.
A flight path indicator uses a visual cue to show relative direction from the current path to the desired path.
A control system adjusts engine valve timing based on residual air fuel mixture detection to regulate fluid flow within the cylinder.
Adjustable exhaust valve with annular protrusions controls back pressure across varying flow rates, reducing system complexity.
Diagnostic system analyzes pressure differences between low and high lift states to detect failed switchable roller finger followers and prevent engine damage.
Opening grill shutters during deceleration pre-cools powertrain components, reducing aerodynamic drag and fuel economy loss during subsequent acceleration.
An actuation signal refusing section ignores repeated switch signals to prevent unnecessary battery consumption.
Phase change material buffers exhaust heat to regenerate aftertreatment devices without adding fuel or restricting airflow.