102:33:03 Aldrin: Altitude light's on.
[In his excellent book, How Apollo Flew To The Moon, David Woods tells us that, when Neil arms the descent engine, two indicator lights on the DSKY come on indicating that the landing radar is not providing adequate data to calculate the LM altitude and rate of descent. Later in the descent, when they get close enough to the surface that the radar is getting good data, those lights will go out.]
102:35:28 Armstrong (onboard): Okay, what do you want? (Garbled) Let's get...Want to get rid of this radar?
102:35:37 Aldrin (onboard): Yeah.
[Fjeld - "Neil is referring to the Rendezvous Radar mode dial, which is in Auto Track and has been since he and Buzz did a post-DOI ranging test - another 'confidence builder'."]
102:35:38 Armstrong (onboard): You're Slew? Okay. (Pause)
[Fjeld - "Here, Neil puts the Rendezvous Radar mode switch in Slew - an action that leads to the Program Alarms and accompanying excitement in the landing. Because the dial is not set at LGC (computer control), once they start getting radar data, the computer will be continuously interrupted with useless (and false) 'warnings' that the radar's CSM tracking angle has changed. The computer will get overloaded five times during the descent and, later, this leads Neil to decide not use the computer for re-targeting the landing site. There was post-flight controversy about the possibility that Neil had made a mistake here, but I think the Crew Procedures Division, misunderstanding or using bad information from MIT, trained the crew that way."]
102:36:11 Armstrong (onboard): Okay, we went by the three-minute point early. We're (going to land) long.
102:36:13 Aldrin: Rate of descent looking real good. Altitude's right about on.
102:36:18 Armstrong: (To Houston) Our position checks down range show us to be a little long.
102:36:21 Duke: Roger. Copy. (Heavy Static)
...There were several interrelated navigation problems, i.e. known deficiencies in the R2 lunar (gravitational) potential model, down-track (along the flight path toward the landing site) and cross-track (left or right, perpendicular to the flight path) propagation errors (errors that start out small but become larger as the flight proceeds), and errors induced by maneuvering of the spacecraft. The principal error induced by maneuvering of the spacecraft was, however, the incomplete vent of the tunnel propagated over one orbit after separation.
[And, finally, Hamish LIndsay, author of Tracking Apollo to the Moon notes that imperfect knowledge of the effects of mascons (mass concentrations) may have also contributed. In 2006, Hamish consulted with Jerry Bostick, who served as Flight Dynamics Officer on Gene Kranz's White Team. Bostick tells us, "It's one of those things that is hard to definitely prove one way or the other, but my opinion is that it was a combination of the tunnel pressure and us not completely understanding - being able to accurately model - the mass concentrations."]
[Armstrong - "We ended up three miles long."]
...However, the downrange position marks after ignition indicated that we were long. Each one that was made indicated that we were 2 or 3 seconds long in range. (That is, they were reaching landmarks 2 or 3 seconds early. One second corresponds to about a mile of miss distance.) The fact that throttle down essentially came on time, rather than being delayed, indicated that the computer was a little bit confused at what our downrange position was. Had it known where it was, it would have throttled down later (to kill a little velocity). Landmark visibility was very good. We had no difficulty determining our position throughout all the face-down phase of powered descent. Correlating with known positions, based on the Apollo 10 pictures, was very easy and very useful."]
However, this delayed it somewhat and, consequently, we were in a slightly lower altitude at the completion of the yaw around than we had expected to be, so we were probably down to about 39,000 or 40,000 feet (altitude) at the time we had radar lockup - as opposed to about 41,500 that we expected to be."]
102:38:25 Duke: That's affirmative.
[They have switched to a data readout which shows Houston the difference between their altitude as determined by the radar and the inertial estimate provided by the PGNS.]
102:38:26 Armstrong: (With the slightest touch of urgency) Program Alarm.
[Armstrong - "I clearly must have said this, and it strikes me as that it's probably right. At least, it was true for me and I think it was for Buzz. We had gone that far and we wanted to land. We didn't want to practice aborts. So I'm sure that we were focusing our attention on doing what was required in order to complete the landing."]
http://next.nasa.gov/alsj/a11/a11.landing.html