Engineering topics
Publications and source records attributed to Diamant, L. S..
To determine whether estimation process simulated by linear error analysis will converge, criterion has been developed based on extension of classical observability. Particular application of technique is with groups of batched navigation data where statistics of estimation errors are derived with classical minimum-variance methods.
Sequential processor performance prediction error with linear method from Monte Carlo cycle analysis of Apollo 14 early rendezvous profile
Detailed specifications and functional flow diagrams for space vehicle entry and landing navigation programs are reported. General design criteria, overall functions, and interfaces between the following three programs are considered: external observations program, noisy observations program, and navigation analysis program.
Return to earth abort capability for Apollo missions for various mission phases