17th Aerospace Sciences Meeting 1979
DOI: 10.2514/6.1979-59
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Guidance laws for short range tactical missiles

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Cited by 11 publications
(6 citation statements)
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“…Once the interceptor receives target estimates from the network, PPN determines the heading angle rate to be applied in order to achieve interception. Conventional PPN was derived assuming no or little delay [1] [7] [8]. In this paper, the same theory is applied provided that the most current target and interceptor states are available through prediction and GPS, respectively.…”
Section: B Ppn With Msp Delay Compensationmentioning
confidence: 99%
See 1 more Smart Citation
“…Once the interceptor receives target estimates from the network, PPN determines the heading angle rate to be applied in order to achieve interception. Conventional PPN was derived assuming no or little delay [1] [7] [8]. In this paper, the same theory is applied provided that the most current target and interceptor states are available through prediction and GPS, respectively.…”
Section: B Ppn With Msp Delay Compensationmentioning
confidence: 99%
“…For a long time, on-board sensors and radars have served as the means to perform target information acquisition in target tracking and interception systems [1]. Due to the significant increase in field visibility, along with many other advantages (such as failure tolerance and integrity), wireless sensor networks (WSNs) have recently been introduced to target tracking and interception applications [2], [3].…”
Section: Introductionmentioning
confidence: 99%
“…However, the guidance systems are suffered with parameter variations, such as target maneuver, missile autopilot and turning rate time constants as well as radome aberration error slope effect (denoted as R in Figure 1). Although some neural methods are also proposed for the design, the tradeoffs of the missile turning rate time constant and radome slope error are hardly included [1][2][3][4][5][6][7]. Figure 2 shows the block diagram of the guidance system, in which R is the radome aberration error slope.…”
Section: Introductionmentioning
confidence: 99%
“…However, for effective intercept, it is of interest to have optimal control on the direction of relative terminal velocity as well as relative terminal position, meanwhile for rendezvous/soft landing problem, the zero relative terminal velocity must be satisfied too. An extensive literature review on guidance laws, in general, and OGLs, in particular has been performed in [9,10].…”
Section: Introductionmentioning
confidence: 99%