Name
Abstract | ||
|---|---|---|
A stochastic computer model was developed to analyze a direct ascent, deep space intercept system. There are two error sources within the system: the deep space tracking system and the launch vehicle guidance system. The errors are modeled based on equipment performance data and analytical results. To compensate for the system errors, the requirements for a maneuverable intercept vehicle are developed. The requirements are described in terms of sensor acquisition distance and vehicle velocity change. Analyses of error sources and tradeoffs amongst maneuver factors are discussed. |
Year | DOI | Venue |
|---|---|---|
1984 | 10.5555/800013.809536 | Winter Simulation Conference |
Field | DocType | Volume |
Computer science,Simulation,Tracking system,Control engineering,Launch vehicle,GPSS,Guidance system,NASA Deep Space Network,Technical report | Conference | 2 |
ISBN | Citations | PageRank |
978-0-911801-11-8 | 0 | 0.34 |
References | Authors | |
0 | 2 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Mark M. Mekaru | 1 | 0 | 0.68 |
| Richard C. Barclay | 2 | 0 | 0.34 |