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Originally posted by telescopeAl
reply to post by eriktheawful
I proved Apollo was a hoax. Because I proved the hoax in general then this video too is a hoax. The video cannot be real if the astronauts cannot navigate to the moon. Ding dong the wicked witch is dead.
Originally posted by telescopeAl
reply to post by Gibborium
Of course we can reach the moon. Rangers were essentially ballistic missiles, no fancy guidance. Surveyors landed.
Originally posted by telescopeAl
reply to post by DJW001
The Apollo computer was not programmed to do this calculation.
The vector a which is used by the IMU alignment programs to correct the stored star vectors for aberration of light is determined as follows:
a=(Vc-Ves)/c
(5.13. 7)
Originally posted by telescopeAl
reply to post by DJW001
In this case of your Apollo 11 you do not know where and how your spaceship is moving because you do not have its precise attitude.
I think the poster was trying to point out that regardless of the ground's ability to track the craft the ship's attitude could not reliably be determined throughout the course of the trip.
Knowing the state vector; position and velocity, that does not mean you can accurately navigate and guide the ship.
Looking at the NASA paper, you can't help but want to read more.
But you are mistaken about the ground's ability to assess attitude.
Such an important point and there seems to be so much confusion about it, seems worth repeating my point in a slightly different way; NASA claimed that determinining an Apollo ship's state vector was most accurately done from the ground with the tracking dishes. But the dishes have absolutely no way to check the accuracy of the ship's attitude. The astronauts aligned the IMU(at least checked it) with their scanning telescope, sextant and AGC. Obtaining values for a state vector and a platform alignment are 2 different things entirely. The former can be done from the ground without any astronaut input. The latter cannot. The IMU alignment is checked in space. IMU alignment must entail star sightings. Otherwise to say one has done it is meaningless. How can you align a platform without reference to your star standard? Once the sightings are made, the ground is given that data and based on the astronauts' work shaft and trunion angles may be sent up. But this is not at all the same as saying the shaft and trunion angles were determined from the state vector. Such a statement would be and is nonsensical. No need to say more, but looks like this is a huge stumbling block for so many here. I wonder why?
Originally posted by DJW001
reply to post by marcomichael
By the poster's own admission, the aberration due to the crafts motion was only about 20 arc-seconds. One arc-second is one sixtieth of one arc-minute. One arc-minute is one sixtieth of a degree. In other words, the error introduced by stellar aberration would be about 1/18 of a degree.
Originally posted by DJW001
reply to post by wmd_2008
Should that not be 1/180 of a degree
Yes, I dropped a zero in my head.
An arsecond is 1/3600 of a degree. So amounts to a little over a curved mile of real estate when dealing with a circle of 240,000 miles radius.