Actuated Automatically TRIZ Cases

See how a landing device with fixed image-capture portions recognizes rotorcraft position from

See how a ground-based landing device with position recognition and remote control enables roto

A single motor and clutch assembly replace dual wheel motors, cutting cleaner size and cost while preserving directional control.

Tracks pilot input rate during flight segments to detect high workload and shift tasks or crew assignments before fatigue and stress rise.

Sensors track pilot stress and workload so flight control can redistribute tasks during critical phases, reducing fatigue and overload.

Alternating ground coverage between solar-powered flight vehicles sustains wireless service while reducing energy use and battery drain.

Analog backup control paths let eVTOL flight controllers maintain pilot command when digital communication to actuators fails.

Non-uniform gust observers from onboard inertial sensors improve control-surface commands to damp aircraft lateral vibrations in turbulence.

Onboard sensors and closed-loop control keep a towed glider on a limit sphere behind the tug to prevent unstable tow termination.

Aircraft status and pilot input patterns are compared to detect spatial disorientation and trigger remedial action during flight.

An independent Lyapunov-based monitor checks aircraft control commands for stability and switches to backup control when instability is detected.

Automated flight guidance engages autopilot and auto-thrust to guide low-visibility landings and execute emergency landing when pilots are incapacitated.

An AI copilot replacement system automates cockpit monitoring and checklists so one onboard pilot can fly safely with remote backup.

Camera-based runway detection corrects heading and state information errors to improve autonomous aerial vehicle flight reliability.

Stacked coaxial ducts with enclosed propulsors and steering flaps improve aerial vehicle efficiency, payload space, and safety.

Virtual copilot controls and ground-based assistance let one onboard pilot access copilot functions while preserving dual-pilot safety.

Retractable control surfaces inside a toroidal ducted UAV redirect airflow for stable roll and pitch control without adding bulk.

Sensors track landing gear force imbalance during taxiing, allowing thrust adjustment to prevent unintended lift-off and keep the aircraft stable.

Real-time allowable-action reporting and danger maps help a base station guide drones to safer locations during emergencies.

Velocity-difference disturbance estimation corrects aircraft target commands to maintain stable guidance and accurate landing in gusts.

Terrain-aware 3D UAV routing limits peak altitude in excess regions, cutting vertical motion and energy use along 2D routes.

Terrain-aware 3D path generation limits UAV altitude exceedance while reducing unnecessary climbs and descents to save energy.

A Lyapunov-based monitoring channel checks whether actuator commands keep the aircraft stable and switches to backup control when instability is detected.

Optical marker sensing gives flying objects precise vertical positioning when satellite signals are unreliable or unavailable.

Preflight checks compare combined order weight, volume, and flight distance with UAV limits to decide batch or split delivery.

Deep reinforcement learning uses flight state and manipulation data to adapt wearable flight control to different user physiques without recalibration.

Mode switching between normal, underpower, and underspeed states keeps full power and pitch control aligned during propulsion shortfalls.

A single-board autonomy layout links GNSS, APNT, and radar directly to processors to cut latency, weight, and improve aerial localization.

Segmented drone flight paths adjust position and boom angle to inspect crane surfaces thoroughly even in narrow work sites.

Pre-stored machine IDs and task templates let a factory UAV generate precise flight plans for autonomous work on specific equipment.

Real-time 3D wind estimation adjusts aircraft control surfaces to limit turbulence-driven path deviation and structural fatigue.

Recorded flight parameters are replayed when GPS, IMU, pressure, or geomagnetic sensors fail, helping stabilize flight and avoid crashes.

Obstacle avoidance is disabled during takeoff, landing, high tilt, or low altitude to prevent false ground detection and unnecessary flight restriction.

Dynamic propulsion derating along a planned vehicle trajectory cuts degradation, emissions, and energy use without losing path performance.

By estimating a target's state from camera images and motor signals, the aircraft can adapt flight actions to avoid attacks, collisions, and missed shots.

A mobile sub-drone tracks the main drone to measure local wind in real time, improving takeoff, landing, and flight stability.

A unified control operator automates thrust distribution in blown lift aircraft to hold flight path angle and reduce pilot workload.

A built-in coordinate conversion unit lets existing numerical controllers send UAV move commands and coordinate aerial tasks with machine tools.

Multiple landing markers of different sizes keep VTOL aircraft aligned to a target point despite altitude changes, rocking, and windblast.

Load sensors detect uneven landing-gear forces and adjust rotor thrust to keep taxiing aircraft grounded and stable.

Sensor-fed flight controllers generate adaptive autopilot outputs to keep electric aircraft stable when pilot control is unavailable.

Landing gear force sensing and attitude feedback help rotorcraft hold steady in gusty landed states while reducing pilot workload.

By receiving unique signals from nearby drones, this case improves long-range position detection without adding heavy multi-direction sensor arrays.

A retrofit piloting architecture links a ground pilot to a pre-existing aircraft, restoring control redundancy when single-pilot emergencies occur.

Complementary filtering removes acceleration drift and smooths relative coordinates so aircraft can hover accurately over moving landing points.

By estimating a target's state from camera or motor signals, the aircraft can hover or ascend to avoid unsafe interaction.

Dynamic input mapping by flight phase lets electric aircraft propulsor controls stay intuitive, improving precision while reducing pilot workload.

A remote pilot takes over cruise control so a single onboard pilot handles only climb, descent, and emergencies on long-range flights.

By positioning between a moving object and a restricted area, the aircraft uses rotor wind to block entry without added deterrent hardware.

Timing-synchronized barometer fusion compensates wind-driven pressure changes, helping UAVs hold altitude and posture when GPS is blocked.

By estimating disturbance from relative and reference velocity gaps, this control approach keeps aircraft navigation stable during gusts.

Real-time display of remaining aircraft control margin helps pilots judge maneuver feasibility and avoid effector saturation.

Real-time display of remaining aircraft control authority uses flight dynamics and effector limits to help pilots avoid input saturation.

Inclination-aware motor speed control lets a drone match sloped landing surfaces and avoid rotational moments during touchdown.

Relative wind sensing aligns VTOL aircraft heading during shipboard takeoff and landing, easing wind restrictions while maintaining safe operation.

Automatic flight guidance selects a suitable airport, flies the approach, and alerts ATC when low visibility or pilot incapacitation makes landing unsafe.

Automatic speed brake control uses speed, altitude, and target data to manage drag during descent, reducing pilot workload and thrust changes.

A rear payload mount with horizontal load retention keeps cargo out of rotor wake, improving flight efficiency and stability in windy conditions.

Regulation module transmits automated control signals to maintain preset tip path plane level and reduce torque requirements during tail rotor failure.

A rotary wing aircraft autopilot switches between trajectory and heading hold modes based on longitudinal speed thresholds.