Direction Controllers TRIZ Cases

See how a second evaporator cools the refrigerant tank to recover vapor, extend refrigerant lif

See how throttling-orifice expansion cools compressible fluid via Joule-Thomson effect to manag

See how throttling-orifice expansion of compressed fluid cools infrared sensors, processors, an

See how a proximity sensor enables airburst capability in laser guided bombs by detecting heigh

Orthogonal 1D transmit and receive arrays on missile control-surface edges improve angular resolution, extend range, and cut radar complexity.

Linear transmit and receive antennas on missile control-surface edges preserve angular resolution while cutting electronics complexity and extending range.

A conical ground chassis nests self-shielded LPA antennas around an EOIR imager to enable passive target geolocation and aimpoint refinement.

Radially distributed antennas on a rotating turret scan azimuth and roll to deliver lighter, lower-complexity radar imaging and detection.

Alternating FMCW and CW radar waveforms let airborne vehicles image terrain and measure velocity accurately without relying on landmarks or GNSS.

An RF antenna substrate with photon-pass openings lets an EOIR sensor share the missile nose, improving targeting accuracy while limiting drag.

Body-mounted strip radar antennas improve target detection and tracking while keeping the missile tip available for other functions.

Parallel sensor channels with integrity checks keep servo-assisted radiation devices operating when a primary sensor or control signal fails.

A segmented Tx/Rx aperture shares one telescope for active transmit and passive receive paths while limiting aberrations and preserving pointing accuracy.

Electronic third-axis scanning removes the zero-site singularity in site-roll radar, improving missile target tracking while cutting motorization and volume.

Radially spaced antennas on a rotating turret scan conical paths to simplify compact radar imaging while detecting object direction, range, and velocity.

An ASE blocks distorted active returns so a gimbaled optical sensor can process passive emissions for open-loop pointing and imaging.

A guidance plane aligns weapon velocity with the target impact vector, cutting glide-energy loss while preserving range and impact direction.

Mode switching lets a UAV leave terminal homing for target search to avoid collateral damage and reassess targets during engagement.

Deep reinforcement learning uses sensor data and hardened FPGA control to keep missile trajectories accurate under weather and interference.

In-flight fusion of lateral acceleration, velocity, and turn rate estimates roll orientation continuously, enabling faster guided-munition engagement.

Ground transmitters and Doppler measurements let a projectile derive motion data for steering or fuze control when GNSS is spoofed or unavailable.

A drone sends target position data to a control station, letting an operator guide the missile without onboard signal detection limits.

Deployable relay transceivers let UAVs maintain stable real-time links beyond line of sight without fixed relay infrastructure.

AI detects likely threat shelters and combines firing probability models with route mapping to prioritize neutralization paths.

Fixed cameras and shaped windows replace gimbals to track aerial targets with lower drag, less weight, and faster launch readiness.

Fixed cameras behind distal and intermediate windows replace gimbals, reducing drag, weight, and launch delay in target tracking.

Deployable transceiver nodes create a self-propagating UAV data link that maintains real-time communication through obstacles without extra infrastructure.

Continuous sensor-based reliability estimation helps crews prevent unsafe aircraft beam emissions by adjusting direction and energy in flight.

Up-finding measurements are fused with inertial data and a Kalman filter to bound drift and sustain navigation accuracy without constant aiding.

Blending skid-to-turn and lower-bandwidth bank-to-turn signals with rudder integrator feedback improves side-force handling and reduces miss distance.

A guidance plane aligns weapon velocity with the target impact vector to cut maneuver energy use and preserve glide range.

Alternating orthogonal actuator commands sweep a tracked missile across its path after track loss, improving field-of-view reacquisition.

Fast angle-of-attack trajectory steering uses precomputed optimal paths to cut onboard computation and enable real-time hypersonic guidance.

A yaw-rotatable camera pod lets a UAV keep positive target identification during sharp turns and approach, reducing exposure time and re-lock risk.

Reinforcement learning steers spin-stabilized projectiles through asymmetric surface rotation, improving accuracy without external fins.

AI maps likely threat shelters on 3D terrain and plans secure routes and unit trajectories within weapon range and autonomy limits.

Separate transmit and receive antennas extend target tracking range while improving resistance to clutter and jamming.

Separate transmit and receive antennas extend tracking range and improve resistance to clutter and jamming for airborne target interception.

Separate transmit and receive antennas extend target tracking range while improving resistance to clutter and jamming for interception.

A calculated guidance bias adjusts flight path in real time so self-propelled flying devices reach targets at the desired time.

Dynamic mode switching lets a UAV leave terminal homing for target search, preserving maneuverability and reducing collateral damage.

Continuous up-finding measurements are fused with inertial data to bound drift and keep vehicle navigation accurate without GPS.

A yaw-adjustable camera pod lets a UAV keep positive target identification through sharp turns, shortening approach time and exposure.

Coordinated salvo geometry and ETA sharing let munitions combine seeker coverage and reach target baskets at nearly the same time in GPS-denied attacks.

Physics-model and upfinding aids correct spin-induced inertial sensor errors, bounding projectile velocity and attitude drift.

UAVs follow estimated projectile paths to capture wind and other conditions aloft, improving firing solutions without static sensors or practice shots.

Shared TWTR range and position data let GPS-denied munitions correct IMU bias drift and maintain accurate target engagement.

Additional gravity bias reshapes rate commands to loft projectile trajectories, extending range and improving terminal impact angle.

An aperture sharing element blocks active signal returns while separating passive emissions, enabling open-loop optical pointing with a common Tx/Rx telescope.

A fixed-sensor guided munition uses a second flight path such as a spiral or U-turn to detect and engage off-axis targets.

Predictive guidance evaluates multiple missile and interceptor trajectories to delay evasive maneuvers, save fuel, and preserve target approach.

A propagator-estimator filter combines projectile dynamics and upfinding roll measurements to bound gyro error growth in velocity and attitude estimates.

Multiple transmitters and Doppler measurements let a projectile determine position or velocity for accurate control when GNSS is unreliable.

Laterally facing coded aperture imaging improves guided munition navigation in GPS-denied flight by correcting inertial drift with terrain and celestial images.

SWIR coded aperture imaging and adaptive masks use celestial, horizon, and terrain cues to correct inertial drift in GPS-denied flight.

Double interpolation on altitude and speed helps launcher guidance stay aligned despite wind shifts and propulsion variation.

Aircraft weapon integration uses generic polynomial coefficients to reconstruct performance envelopes, reducing data storage and processing needs.