Actuated Automatically TRIZ Cases

Servo actuators actuate flight control surfaces to verify gust lock status before engine start.

A monitoring device analyzes guidance instructions to identify defective flight management systems.

Dynamic phase lag compensation prevents off-axis moments during flight maneuvers.

Independent flap positioning via a single drive link optimizes lift-drag tradeoffs, reducing fuel consumption and noise during takeoff and landing.

A breakable link merges dual yoke inputs to enable remote pilot assistance, reducing operational complexity and personnel requirements.

Segmented control systems adapt aileron and spoiler deflection to gust length, resolving the trade-off between peak load reduction and control authority.

Closure panel bridges gap between wing and control surface, eliminating aerodynamic disturbances caused by movable flight surfaces.

A delivery rotary-wing aircraft uses an adjustable supporting member to vertically extend the package mounting portion and shift the center of gravity downward.

Inertial sensor fusion replaces optical horizon detection to maintain safe flight envelopes in cloudy or indoor environments.

Flight control system generates bank commands to maintain a circular groundtrack around a geospatial point using sensor data.

An obstacle detecting unit triggers lift deployment to decelerate the flying body and mitigate collision impact.

Segmented modules and universal interfaces enable full-envelope automation across take-off, cruise, and landing phases without permanent integration.

Actuators adjust aileron uprig positions to eliminate additional fuel requirements while maintaining differential deflection capability.

Movable compression surfaces dynamically adjust position to reduce steep pressure gradients and sonic boom magnitude across varying operational conditions.

A rotorcraft control system detects ground reaction forces to switch between flight and ground laws while maintaining active integrators.

Independent wheel actuators adjust rotational speeds dynamically, reducing turning time and friction while maintaining high maneuverability.

Signal processing unit calculates a reliability index by comparing Doppler shift amounts from multiple integrated data sets.

An effector controller performs diagnostic tests during flight to manage system reliability.

Orthogonal magnetic detectors measure field strength to determine AGV position along weak passive markers.

Parallel integration validates persistent asymmetry to eliminate spurious braking while maintaining critical response speed.

Processor calculates optimal deflection angles from live altitude and speed data, reducing fuel consumption by overcoming static table limitations.

Auxiliary wheels push against the floor to overcome static friction, reducing actuator power needs.

Laser beam locating sensors detect wing position on aircraft structures to enable active twist correction mechanisms.

A controller generates and transmits battery parameter sets to optimize electric aircraft charging efficiency.

A radio-controlled UAV uses a parachute and suspended control module to enable precise maneuvering with minimal operator training.

Information processing apparatus manages arrival time using probability distributions of uncertain predicted values.

A rotary wing flight control system uses dedicated axes to modify forward speed and course angles independently via an autopilot.

Aerial craft detect energized power lines using electric and magnetic field sensors to determine line orientation for autonomous navigation.

Force feedback monitors spoiler contact stiffness to maintain aerodynamic sealing, reducing drag and structural loads on the flap.

Automatic leading edge slat deployment increases lift to counter ice-induced stall margin reduction during critical climb phases.

Automated high lift control system manages slat and flap positioning through discrete selector inputs.

Angle-of-attack thresholds automatically adjust aircraft high lift device configurations without relying on conventional speed sensors.

Avionics trigger aerodynamic drag via slip maneuvers to manage over-speed conditions without consuming extra fuel or deploying speed brakes.

Actuators dynamically reshape surfaces to cancel resonance and reduce drag, addressing insufficient control effectiveness in crosswinds.

Determining a switch-over vertical point by integrating dynamic flight equations to resolve prediction accuracy issues during manual-to-guided mode transitions.

A piloting aid device uses a postero-anterior camera to identify desired landing zones for rotorcraft approach.

A HAPS laser relay network forms a three-dimensional mesh topology to resolve propagation delay and system complexity in wide-area 5G IoT coverage.

Merging a camera with a laser ranging system reduces surveillance weight while maintaining precise distance measurement for midair collision avoidance.

A grooved aircraft wing structure guides a pivotable flap carriage along its length using a single actuator to position the trailing edge.

Pre-positioned propulsors with offset rotational axes generate counteracting torque to maintain aircraft safety during component failures.

Multi-level corpus data augmentation generates diverse acoustic training samples for aircraft speech recognition models.

A proactive vehicle control system predicts environmental forces to adjust operating parameters.

A control method adjusts hybrid helicopter wing flaps to optimize main rotor pitch during stabilized flight phases.

Autonomous controller detects landing gear malfunctions and initiates remedial actions, reducing pilot workload during critical operations.

Autopilot switches between ground and air speed setpoints using wind feedback to prevent vortex ring states during flight.

Unified touchscreen and yoke controls reduce switch mass and wiring complexity while improving pilot ergonomics and manipulation speed.

A fault-tolerant control system switches to a backup mode when UAV aerodynamic surfaces fail.

Aircraft aerodynamic angle detection system adjusts inertial and external signal contributions to reduce noise.