Improved Parallel-Structured Newton-Type Guidance for Launch Vehicles Under Thrust Drop Fault
2021
When launch vehicles encounter thrust drop f4aults during endoatmospheric flight, conventional nominal trajectory-based guidance methods may fail to compensate adequately; and the launch mission ma...
- Correction
- Source
- Cite
- Save
- Machine Reading By IdeaReader
33
References
1
Citations
NaN
KQI