ETTC'2003 - SEE

ETTC'2003 - SEE ETTC'2003 - SEE

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BACK STUDY OF 3∆t PASSIVE LOCATING SYSTEM Xie Nan and Chen Da-Hai Electronic Engineering Institute of China Academy of Engineering Physics P.O.BOX 919-517, Mianyang, Sichuan, P.R.China Zip Code: 621900 Tel: +86 816 2487524 Fax: +86 816 2487594 E-mail:xienanlx@hotmail.com ABSTRACT The reentry low altitude vehicle locating technology based on 3∆t passive locating principles is discussed in this paper. At first its basic principle is introduced, and we discuss the sources of errors in the existing telemetry system and corresponding precision. Some methods, which are used to improve the precision, are proposed at the end of this paper. KEY WORDS Reentry, Telemetry System, 3∆t Passive Locating, Error INTRODUCTION In the reentry measurement, one of our missions is to measure the track and the point of fall of the reentry vehicle. It can be named reentry-locating technology. In general, radar can be used to locate the track and the point of fall of aircraft. It locates the position of aircraft by measuring the azimuth, the elevation and the distance. The optical measurement is also used sometimes. The precision and the accuracy of these methods are satisfying. In the reentry-locating measurement, the reentry vehicle is different from any other aircrafts. During the reentry, it will pass the blackout area. The telecommunication will be interrupted in this area. After the vehicle going out of the area, the speed of it is very high and the altitude is very low. So above-mentioned systems can’t capture the target before it fell to the ground. These systems are not suitable for the reentry vehicle track measurement. Another system, which is called 3R-locating system, can be used in the track measurement of reentry vehicle. It needs at least three ground stations A, B, C and locates the position of vehicle by measuring the distance between the vehicle and each of the respective stations. The stations sent query signals to reentry vehicle and received the responses. The time of propagation from each of the respective stations to the vehicle, i.e., the time to travel the distances, , and r , are computed. The distance r C r is rA B given by r = τ ⋅ c , where c is the velocity of light. Then the position can be located. This system works in active mode. The result of test is not satisfying. So we need a useful system to realize the locating of reentry vehicle. In this paper, the 3∆t passive locating system is introduced. It needs at least four ground stations. In this system, the ground stations don’t send any signals; they receive the common telemetry signal, for example the frame synchronization signal, from the reentry vehicle and record the time of arrival. Because the time when the signal was sent is unknown, one more station is needed in 3∆t system than in 3R system. Three time differences are given by ∆ ti = ti − ti+ 1 , ( i = 1, 2, 3) , where ti is the time of

arrival. The coordinates of four ground stations are known, and then the position of the reentry vehicle can be computed. For the 3∆t system working in passive mode, it can make use of the existing telemetry system. No more equipment is needed in reentry vehicle. Only one time-recorder is needed in each of ground stations. It is one of its advantages that the system is simple. PRINCIPLE OF 3∆t SYSTEM Fig 1. Shows the composition of 3∆t passive locating system. The ground stations receive the GPS Satellite ground stations reentry vehicle Fig 1. the 3Δt passive locating system common telemetry signal sent from reentry vehicle, and record the time of arrival respectively, then r1 t1 = T0 + c r2 t2 = T0 + c (1) M t N rN = T0 + c where ( i 1, 2, L, N) is the time of arrival, T is the time of signal sent, ( i = 1, 2, L, N) is the t i distance between ground stations and reentry vehicle respectively, c is the velocity of light in meters per second. = 0 Provided that the coordinates of ground station is [ ] T x , y , z XT = T T T , then For the T0 is unknown, then i [ ] T x , y , z Xi i i i r − r i = , the coordinates of target is 2 2 2 2 i = ( xT − xi ) + ( yT − yi ) + ( zT zi ) (2)

arrival. The coordinates of four ground stations are known, and then the position of the reentry vehicle<br />

can be computed. For the 3∆t system working in passive mode, it can make use of the existing telemetry<br />

system. No more equipment is needed in reentry vehicle. Only one time-recorder is needed in each of<br />

ground stations. It is one of its advantages that the system is simple.<br />

PRINCIPLE OF 3∆t SYSTEM<br />

Fig 1. Shows the composition of 3∆t passive locating system. The ground stations receive the<br />

GPS Satellite<br />

ground stations<br />

reentry vehicle<br />

Fig 1. the 3Δt passive locating system<br />

common telemetry signal sent from reentry vehicle, and record the time of arrival respectively, then<br />

r1<br />

t1<br />

= T0<br />

+<br />

c<br />

r2<br />

t2<br />

= T0<br />

+<br />

c<br />

(1)<br />

M<br />

t<br />

N<br />

rN<br />

= T0<br />

+<br />

c<br />

where ( i 1,<br />

2,<br />

L,<br />

N)<br />

is the time of arrival, T is the time of signal sent, ( i = 1,<br />

2,<br />

L,<br />

N)<br />

is the<br />

t i<br />

distance between ground stations and reentry vehicle respectively, c is the velocity of light in meters<br />

per second.<br />

= 0<br />

Provided that the coordinates of ground station is<br />

[ ] T<br />

x , y , z<br />

XT = T T T<br />

, then<br />

For the T0<br />

is unknown, then<br />

i [ ] T<br />

x , y , z<br />

Xi i i i<br />

r −<br />

r i<br />

= , the coordinates of target is<br />

2<br />

2<br />

2<br />

2<br />

i = ( xT<br />

− xi<br />

) + ( yT<br />

− yi<br />

) + ( zT<br />

zi<br />

)<br />

(2)

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