Onboard midcourse correction targeting during the transearth coast phase of a lunar mission. Project Apollo
Onboard midcourse correction targeting during transearth phase of lunar mission
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Onboard midcourse correction targeting during transearth phase of lunar mission
Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 data
Spatial bias correction for sporadic meteors photographed in New Mexico
Spacecraft trajectory correction propulsion system
Sonic boom overpressures generated by aircraft level rectilinear flight at supersonic speed in temperature and wind stratified atmosphere, calculating atmospheric correction factor
Apollo onboard computers tracking data state- vector corrections covariance matrix, considering initial estimate, noise and tracking geometry errors
Mangler displacement thickness correction for slender cones
Coupled Schroedinger equations for diatomic molecules internal motion solved using best adiabatic approximation to obtain energy correction to Born-Oppenheimer method
Interplanetary midcourse velocity correction schedules optimization, discussing timing equations modifications, mission simulation and role of earth based radar
Atmospheric refractive corrections in high accuracy radio interferometry
Bit error probability after decoding for binary perfect single error correcting codes
Time response deviation correction in hybrid computer control systems with digital feedback elements containing quantized coefficients
Navigation correction systems for space missions, discussing prelaunch analysis, design and mission operations, hardware, etc
Correction techniques for thermal network lumped parameter inaccuracies with conduction and radiation coupling, considering temperature control system
Adiabatic corrections to long range Born- Oppenheimer interatomic potentials from rotationally coupled Schroedinger equations
Closed form expressions for linear and higher order corrections to multiimpulse approximations of space flight trajectory optimization solutions, using bang-bang thrust control
Unit distance redundant counting code for single error correction or double error detection with digital equipment simplicity advantages
Beam squint is eliminated by using received phase at each array element to control transmitted phase at another element. Correction method may extend to multi-element array by using ring structure.