Výsledky vyhledávání - "Guidance and Trajectory Optimization Algorithms"

A Unified, Configurable, Non-Iterative Guidance System For Launch Vehicles

Autoři: Rajeev, U P

Thesis Advisors: Bhat, M Seetharama

Témata: Launch Vehicle, Guided Missiles, Trajectory Optimization, Guidance and Trajectory Optimization Algorithms, Closed Loop Guidance Algorithms, Launch Vehicles - Guidance Algorithms, Flat Earth Guidance, Predicted Target Flat Earth (PFE), Classical Flat Earth (CFE), Military Engineering

Relation: G20927

Dostupnost: http://hdl.handle.net/2005/1065

A Unified, Configurable, Non-Iterative Guidance System For Launch Vehicles

Autoři: Rajeev, U P Bhat, M Seetharama

Přispěvatelé: Rajeev, U P Bhat, M Seetharama

Témata: Launch Vehicle, Guided Missiles, Trajectory Optimization, Guidance and Trajectory Optimization Algorithms, Closed Loop Guidance Algorithms, Launch Vehicles - Guidance Algorithms, Flat Earth Guidance, Predicted Target Flat Earth (PFE), Classical Flat Earth (CFE), Military Engineering

Popis souboru: application/pdf

Relation: G20927; https://etd.iisc.ac.in/handle/2005/1065

Dostupnost: https://etd.iisc.ac.in/handle/2005/1065