PAJ GPS POWER Finder- Magnet Mount GPS Tracker- Tracking Device for Cars, Machinery, Boats- 40 Days’ Battery while active and up to 90 Days in Stand by- Real-time Tracker with Antitheft Protection
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PAJ GPS POWER Finder- Magnet Mount GPS Tracker- Tracking Device for Cars, Machinery, Boats- 40 Days’ Battery while active and up to 90 Days in Stand by- Real-time Tracker with Antitheft Protection
- Brand: Unbranded
PAJ GPS POWER Finder- Magnet Mount GPS Tracker- Tracking Device for Cars, Machinery, Boats- 40 Days’ Battery while active and up to 90 Days in Stand by- Real-time Tracker with Antitheft Protection
- Brand: Unbranded
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Description
Satellite data is updated typically every 24 hours, with up to 60 days data loaded in case there is a disruption in the ability to make updates regularly. Typically the updates contain new ephemerides, with new almanacs uploaded less frequently. The Control Segment guarantees that during normal operations a new almanac will be uploaded at least every 6 days. The GPS satellites (called space vehicles in the GPS interface specification documents) transmit simultaneously several ranging codes and navigation data using binary phase-shift keying (BPSK). An ephemeris is valid for only four hours; an almanac is valid with little dilution of precision for up to two weeks. [7] The receiver uses the almanac to acquire a set of satellites based on stored time and location. As each satellite is acquired, its ephemeris is decoded so the satellite can be used for navigation. The C/A code is transmitted on the L1 frequency as a 1.023MHz signal using a bi-phase shift keying ( BPSK) modulation technique. The P(Y)-code is transmitted on both the L1 and L2 frequencies as a 10.23MHz signal using the same BPSK modulation, however the P(Y)-code carrier is in quadrature with the C/A carrier (meaning it is 90° out of phase).
Since the FEC encoded bit stream runs at 2 times the rate than the non FEC encoded bit as already described, then t = ⌊ t ′ 2 ⌋ {\displaystyle t=\left\lfloor {\tfrac {t'}{2}}\right\rfloor } . FEC encoding is performed independently of navigation message boundaries; [27] this follows from the above equations.GPS signals include ranging signals, used to measure the distance to the satellite, and navigation messages. The navigation messages include ephemeris data, used in trilateration to calculate the position of each satellite in orbit, and information about the time and status of the entire satellite constellation, called the almanac. The second advancement is to use forward error correction (FEC) coding on the NAV message itself. Due to the relatively slow transmission rate of NAV data (usually 50 bits per second), small interruptions can have potentially large impacts. Therefore, FEC on the NAV message is a significant improvement in overall signal robustness. For the ranging codes and navigation message to travel from the satellite to the receiver, they must be modulated onto a carrier wave. In the case of the original GPS design, two frequencies are utilized; one at 1575.42 MHz (10.23MHz × 154) called L1; and a second at 1227.60MHz (10.23MHz × 120), called L2. In each subframe, each hand-over word (HOW) contains the most significant 17 bits of the TOW count corresponding to the start of the next following subframe. [14] Note that the 2 least significant bits can be safely omitted because one HOW occurs in the navigation message every 6 seconds, which is equal to the resolution of the truncated TOW count thereof. Equivalently, the truncated TOW count is the time duration since the last GPS week start/end to the beginning of the next frame in units of 6 seconds.
The P-code is a PRN sequence much longer than the C/A code: 6.187104x10 12 chips. Even though the P-code chip rate (10.23 Mchip/s) is ten times that of the C/A code, it repeats only once per week, eliminating range ambiguity. It was assumed that receivers could not directly acquire such a long and fast code so they would first "bootstrap" themselves with the C/A code to acquire the spacecraft ephemerides, produce an approximate time and position fix, and then acquire the P-code to refine the fix. The arguments of the functions therein are the number of bits or chips since their epochs, starting at 0. The epoch of the LFSRs is the point at which they are at the initial state; and for the overall C/A codes it is the start of any UTC second plus any integer number of milliseconds. The output of LFSRs at negative arguments is defined consistent with the period which is 1,023 chips (this provision is necessary because B may have a negative argument using the above equation).The modulation method is binary offset carrier, using a 10.23MHz subcarrier against the 5.115MHz code. This signal will have an overall bandwidth of approximately 24MHz, with significantly separated sideband lobes. The sidebands can be used to improve signal reception. The project involves new ground stations and new satellites, with additional navigation signals for both civilian and military users, and aims to improve the accuracy and availability for all users. A goal of 2013 was established with incentives offered to the contractors if they can complete it by 2011. The L5 band provides additional robustness in the form of interference mitigation, the band being internationally protected, redundancy with existing bands, geostationary satellite augmentation, and ground-based augmentation. The added robustness of this band also benefits terrestrial applications. [30]
Having reached full operational capability on July 17, 1995 [20] the GPS system had completed its original design goals. However, additional advances in technology and new demands on the existing system led to the effort to "modernize" the GPS system. Announcements from the Vice President and the White House in 1998 heralded the beginning of these changes and in 2000, the U.S. Congress reaffirmed the effort, referred to as GPS III. L1C is a civilian-use signal, to be broadcast on the L1 frequency (1575.42MHz), which contains the C/A signal used by all current GPS users. The L1C signals will be broadcast from GPS III and later satellites, the first of which was launched in December 2018. [1] As of January2021 [update], L1C signals are not yet broadcast, and only four operational satellites are capable of broadcasting them. L1C is expected on 24 GPS satellites in the late 2020s. [1] The delay for PRN numbers 34 and 37 is the same; therefore their C/A codes are identical and are not transmitted at the same time [5] (it may make one or both of those signals unusable due to mutual interference depending on the relative power levels received on each GPS receiver). The interface to the User Segment ( GPS receivers) is described in the Interface Control Documents (ICD). The format of civilian signals is described in the Interface Specification (IS) which is a subset of the ICD. The P code is public, so to prevent unauthorized users from using or potentially interfering with it through spoofing, the P-code is XORed with W-code, a cryptographically generated sequence, to produce the Y-code. The Y-code is what the satellites have been transmitting since the anti-spoofing module was set to the "on" state. The encrypted signal is referred to as the P(Y)-code.L1C consists of a pilot (called L1C P) and a data (called L1C D) component. [35] These components use carriers with the same phase (within a margin of error of 100 milliradians), instead of carriers in quadrature as with L5. [36] The PRN codes are 10,230 chips long and transmitted at 1.023Mchip/s, thus repeating in 10ms. The pilot component is also modulated by an overlay code called L1C O (a secondary code that has a lower rate than the ranging code and is also predefined, like the ranging code). [35] Of the total L1C signal power, 25% is allocated to the data and 75% to the pilot. The modulation technique used is BOC(1,1) for the data signal and TMBOC for the pilot. The time multiplexed binary offset carrier (TMBOC) is BOC(1,1) for all except 4 of 33 cycles, when it switches to BOC(6,1). Pre-operational signal with message set "unhealthy" until sufficient monitoring capability established C/A i is the code with PRN number i. A is the output of the first LFSR whose generator polynomial is x → x 10 + x 3 + 1, and initial state is 1111111111 2. B is the output of the second LFSR whose generator polynomial is x → x 10 + x 9 + x 8 + x 6 + x 3 + x 2 + 1 and initial state is also 1111111111 2. D i is a delay (by an integer number of periods) specific to each PRN number i; it is designated in the GPS interface specification. [4] ⊕ is exclusive or. X 1 ( t ) = d ( t ) ⊕ d ( t − 2 ) ⊕ d ( t − 3 ) ⊕ d ( t − 5 ) ⊕ d ( t − 6 ) X 2 ( t ) = d ( t ) ⊕ d ( t − 1 ) ⊕ d ( t − 2 ) ⊕ d ( t − 3 ) ⊕ d ( t − 6 ) d ′ ( t ′ ) = { X 1 ( t ′ 2 ) if t ′ ≡ 0 ( mod 2 ) X 2 ( t ′ − 1 2 ) if t ′ ≡ 1 ( mod 2 ) {\displaystyle {\begin{aligned}X_{1}(t)&=d(t)\oplus d(t-2)\oplus d(t-3)\oplus d(t-5)\oplus d(t-6)\\X_{2}(t)&=d(t)\oplus d(t-1)\oplus d(t-2)\oplus d(t-3)\oplus d(t-6)\\d'(t')&={\begin{cases}X_{1}\left({\frac {t'}{2}}\right)&{\text{if }}t'\equiv 0{\pmod {2}}\\X_{2}\left({\frac {t'-1}{2}}\right)&{\text{if }}t'\equiv 1{\pmod {2}}\\\end{cases}}\end{aligned}}} The L1C pilot and data ranging codes are based on a Legendre sequence with length 10 223 used to build an intermediate code (called a Weil code) which is expanded with a fixed 7-bit sequence to the required 10,230 bits. This 10,230-bit sequence is the ranging code and varies between PRN numbers and between the pilot and data components. The ranging codes are described by: [37] L1C i ( t ) = L1C ′ ( t mod 10 230 ) L1C i ′ ( t ′ ) = { W i ( t ′ ) if t ′ < p i ′ S ( t ′ − p i ′ ) if p i ′ ≤ t ′ < p i ′ + 7 W i ( t ′ − 7 ) if t ′ ≥ p i ′ + 7 S = ( 0 , 1 , 1 , 0 , 1 , 0 , 0 ) W i ( n ) = L ( n ) ⊕ L ( ( n + w i ) mod 10 223 ) L ( n ) = { 1 if n ≠ 0 and there is an integer m such that n ≡ m 2 ( mod 10 223 ) 0 otherwise {\displaystyle {\begin{aligned}{\text{L1C}}_{i}(t)&={\text{L1C}}'(t{\bmod {10\,230}})\\{\text{L1C}}'_{i}(t')&={\begin{cases}W_{i}(t')&{\text{ if }}t'
A and B are maximal length LFSRs. The modulo operations correspond to resets. Note that both are reset each millisecond (synchronized with C/A code epochs). In addition, the extra modulo operation in the description of A is due to the fact it is reset 1 cycle before its natural period (which is 8,191) so that the next repetition becomes offset by 1 cycle with respect to B [32] (otherwise, since both sequences would repeat, I5 and Q5 would repeat within any 1ms period as well, degrading correlation characteristics). General features [ edit ] A visual example of the GPS constellation in motion with the Earth rotating. Notice how the number of satellites in view from a given point on the Earth's surface, in this example at 45°N, changes with time. A major component of the modernization process is a new military signal. Called the Military code, or M-code, it was designed to further improve the anti-jamming and secure access of the military GPS signals.Besides redundancy and increased resistance to jamming, a critical benefit of having two frequencies transmitted from one satellite is the ability to measure directly, and therefore remove, the ionospheric delay error for that satellite. Without such a measurement, a GPS receiver must use a generic model or receive ionospheric corrections from another source (such as the Wide Area Augmentation System or WAAS). Advances in the technology used on both the GPS satellites and the GPS receivers has made ionospheric delay the largest remaining source of error in the signal. A receiver capable of performing this measurement can be significantly more accurate and is typically referred to as a dual frequency receiver. There are two navigation message types: LNAV-L is used by satellites with PRN numbers 1 to 32 (called lower PRN numbers) and LNAV-U is used by satellites with PRN numbers 33 to 63 (called upper PRN numbers). [9] The 2 types use very similar formats. Subframes 1 to 3 are the same [10] while subframes 4 and 5 are almost the same. Each message type contains almanac data for all satellites using the same navigation message type, but not the other. In addition to the PRN ranging codes, a receiver needs to know the time and position of each active satellite. GPS encodes this information into the navigation message and modulates it onto both the C/A and P(Y) ranging codes at 50bit/s. The navigation message format described in this section is called LNAV data (for legacy navigation). It uses forward error correction (FEC) provided by a rate 1/2 convolutional code, so while the navigation message is 25-bit/s, a 50-bit/s signal is transmitted.
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