Explicit guidance equations are derived for use with a variable trim reentry vehicle. With a simplifying assumption the equations can be put in a cross product form. Preliminary simulation results have demonstrated the feasibility of the proposed guidance equations. (Author)
Explicit Guidance Equations for a Variable Trim Reentry Vehicle
1978
23 pages
Report
No indication
English
Missile Guidance & Control Systems , Missile Trajectories & Reentry Dynamics , Guided missile trajectories , Command guidance , Reentry vehicles , Flight paths , Atmosphere entry , Equations , Approach , Lift , Maneuverable reentry vehicles , Ballistic trajectories , Guided missile targets , Surface targets , Missile guidance , Variable lift reentry vehicles
Trim aerodynamics of a warped reentry vehicle
AIAA | 1980
|Optimal Nonlinear Guidance for a Reentry Vehicle
British Library Online Contents | 1992
|