Program: P66 Landing Phase (ROD)
Purpose: To control the LM in final phase of landing. With Mode Control in
Auto
forward and lateral velocities are nulled. When in Manual the inertial
attitude is
controlled by the astronaut. Throttle is calculated and Rate of Descent (ROD)
is
controlled by toggling the ROD switch.
P66 is started automatically by Landing Auto Modes Monitor routine when
targeted
conditions for P64 are met or the ROD switch has been activated after P63.
Displays and Actions
Flashing Forward
Velocity
XXXX.X ft/s
V06N60 Altitude Rate
XXXX.X ft/s
Computed Altitude
XXXXX ft
Use ROD switch as desired.
To manually null forward and lateral velocities: Mode Control: PGNS > Attitude
Hold.
Manual throttle available
V16N92E
Flashing Percent Full Thrust 00XXX ft/s
V16N92 Altitude Rate XXXX.X ft/s
Computed Altitude XXXXX ft
KEY REL
Flashing Forward Velocity XXXX.X ft/s
V06N60 Altitude Rate XXXX.X ft/s
Computed Altitude XXXXX ft
Engine Stop
PRO
Next Program is Landing Confirmation Program P68:,WHITE
V37E68E