Direction Controllers TRIZ Cases

Transferring error data to non-volatile memory preserves diagnostic information after carrier aircraft power loss, enabling post-flight analysis.

Spatial filtering of modulated CW laser signals through image sensor arrays enables daylight detection without high peak power pulsed lasers.

Segmenting delay paths within a reconfigurable optical waveguide network resolves timing precision versus device complexity contradictions in ladar testing.

An asymmetric formation on the rotating nose portion creates off-axis drag, resolving mechanical deformation risks from radial canards during barrel passage.

Segmented head modules with interchangeable guidance assemblies resolve versatility versus complexity trade-offs in underwater targeting systems.

Magnetic coupling replaces mechanical linkages in a steerable antenna, reducing device complexity while maintaining measurement precision.

Fast steering mirrors steer beacon illuminator beams to correct atmospheric jitter, maximizing power-on-target and improving signal-to-noise ratios.

An embedded control zone decouples touch input from the display area, maintaining target visibility while enabling precise aiming.

Segmented flash detector array resolves targeting precision limits in semi-active laser systems by enabling spatial signal detection.

A ball joint gimbal imaging system relays optical apertures using two-axis steering elements to align light with an off-gimbal electro-optic component.

An unscented Kalman filter processes geometrically diverse sensor measurements to track hypersonic objects across boost, ballistic, and glide phases.

A polyolefin-based protective dome transmits infrared and radio frequency radiation through its specific material composition.

Digital processor calculates compensated sum and difference signals from functioning receive channels.

A filter substrate integrates polarization and multispectral filters to analyze electromagnetic radiation signatures from ground targets.

A targeting system uses a remote fire control to transmit coordinate offsets for mid-course projectile guidance.

Loop-closure algorithms correct IMU drift errors to determine precise positions in occluded aircraft areas.

A stochastic mission planning system selects optimal engagement paths using precomputed behavioral logic tables derived from real-time sensor inputs.

A portable verification device decodes reflected laser signals to identify targets without platform integration.

A determination apparatus compares pre-calculated expected missile trajectories against stored topographic elevation data to assess launch path safety.

A Vehicle Based Independent Range System uses satellite modules to enable simultaneous launch vehicle tracking and data gathering.

Assigns moving vehicles to launcher systems using real-time position data and predicted trajectories.

A matrix detector calculates subtraction signals between consecutive time windows to process electromagnetic pulses for precise target localization.

A guidance control method generates optimal commands using swarm optimization algorithms to navigate a pursuer toward a target.

An automated system processes in-flight seeker video to compute optimized aimpoints for missile targeting.

A remote aerial vehicle system updates pointing commands using stored flight parameters to guide the platform toward a designated target.

Unmanned aerial vehicles navigate segmented ballistic flight paths to capture precise environmental data points along the projectile trajectory.

A control device manages missile simulation and test procedures through automated program execution.

A feed forward guidance kit uses optical sensors and a processor to proactively calculate anticipated target positions based on orientation changes.

Segmented detectors with adjacent amplifiers reduce wire interference and capacitance to improve signal-to-noise ratio.

A Launch Acceptability Region display system generates simultaneous visual representations of multiple regions based on varying input parameters.

Segmenting guidance into unresolved and resolved phases improves time-to-go estimation accuracy by switching from irradiance to area measurements.

System compensates for sensor data time lag by calculating state transitions as functions of estimated latency to improve prediction accuracy.

Interface assemblies translate legacy serial bus messages into standard Ethernet protocols, resolving module interchangeability bottlenecks in munitions.

Nested pulleys and rigid metal bands resolve the trade-off between high transmission precision and bulky volume in missile seeker antennas.

An asymmetric laser beam illuminates the missile and control unit, resolving range limitations in countermeasure systems.

Disposable air brake creates separation distance from intercepting objects, allowing the guided projectile to resume its target trajectory after evasion.

A compressed fluid launcher uses a wound blade deploying along an axis to propel projectiles.

Add-on kit guides munitions without structural modification by using GPS data to adjust wing angles.

Modifies attitude commands to steer boresight around exclusion zones, preventing high rates that extend tracking compromise.