Optimal explicit guidance for three-dimensional launch trajectory

Author:

Sinha S.K.,Shrivastava S.K.,Bhat M.S.,Prabhu K.S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

1. Closed loop guidance of satellite launch vehicle—an overview;Shrivastava;J. Inst. Engrs India,1986

2. Space guidance evolution—a personal narrative;Battin;J. Guid. Control,1982

3. A class of unified explicit methods for steering throttlable and fixed thrust rocket;Cherry;Prog. Astronaut. Aeronaut. Guid. Control II,1964

4. Development of iterative guidance mode with its application to various vehicles and missions;Chandler;J. Spacecraft Rockets,1967

5. Saturn launch vehicle's navigation, guidance and control system;Haeussermann;Automatica,1971

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