The Malcolm D. Shuster Astronautics Symposium: Proceedings of the University at Buffalo, State University of New York/AAS Malcolm D. Shuster Astronautics Symposium Held June 12-15, 2005, Grand Island, New YorkJohn L. Crassidis American Astronautical Society, 2006 - 606 Seiten |
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Seite 5
... mean biases and variances . 3. Estimate and remove time - varying measurement residual biases in real time . 4 ... mean . 2. Gaussian white residuals with zero mean imply Gaussian white state estimate errors with zero mean ( due to ...
... mean biases and variances . 3. Estimate and remove time - varying measurement residual biases in real time . 4 ... mean . 2. Gaussian white residuals with zero mean imply Gaussian white state estimate errors with zero mean ( due to ...
Seite 18
... mean squared state error will be minimized for each component 16 of the state estimate . Theorem 3 invokes the ... mean - squared errors . 9 9.1 An Operational Proceedure to Minimize Mean- Squared State Error Gaussian Distribution ...
... mean squared state error will be minimized for each component 16 of the state estimate . Theorem 3 invokes the ... mean - squared errors . 9 9.1 An Operational Proceedure to Minimize Mean- Squared State Error Gaussian Distribution ...
Seite 241
... mean quaternion estimation error of 1000 Monte Carlo runs of the three filters . This Figure explicitly illustrates the role of the adaptive scheme . Without any knowledge of the true TAM pdf , the adaptive GA - QPF reaches steady ...
... mean quaternion estimation error of 1000 Monte Carlo runs of the three filters . This Figure explicitly illustrates the role of the adaptive scheme . Without any knowledge of the true TAM pdf , the adaptive GA - QPF reaches steady ...
Inhalt
Solutions to the Multidimensional Nonlinear RealTime | 3 |
A Simple Globally Convergent Three Axis Attitude Observer Using Rate Data | 29 |
Satellite Electricity on Orbital Time Scales AAS 05454 | 51 |
Urheberrecht | |
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AAS Microfiche Series AAS/AIAA algorithm ambiguities angle antennas applied Argument of Latitude Astrodynamics Astronautical Sciences attitude determination attitude estimation axis b₁ baselines Brazilian Brazilian space program calibration Cayley form components computed constraints Control coordinates cost function covariance matrix Cover $45 ISBN defined denote developed dynamics eigenvalue Engineering equations estimate error Figure fuel Gaussian given gyro gyrostat Hamiltonian Hard Cover hypersphere initial conditions INPE integration Journal of Guidance Kalman filter linear logarithmic spiral M. D. Shuster maneuver Markley measurement model method Microfiche Microfiche Suppl motion orbit orbit frame orthogonal paper parameters particle particle filter Phase-I pixel plane problem propagation quaternion quaternion estimate QUEST refueling representation RNEW rotation samples satellite sensor simulation Soft Cover solution space spacecraft Spacecraft Attitude stochastic Symposium Theorem trajectory true anomaly update variables Vector Observations Vlim zero